Job Title: Space Vehicle Integration and Test Systems Engineer (Active TS/SCI Clearance Required) Job Code: 10692 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Integration and Test systems engineer (I&T SE) to join our growing team. The individual in this role will act as the primary integration and test systems engineer responsible for coordinating and overseeing verification and test planning for the integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The I&T SE has overall technical responsibility for the design and development of the test plan and flow for the Space Vehicle as well as ownership of the Test Bed and Simulators. The I&T SE serves as the primary point of contact between the SV Engineering team and the Assembly, Integration, and Test (AIT) execution and operations team and coordinates major integration and test activities. The I&T SE will coordinate all integration and test technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Develops, manages and maintains the verification and test plans and procedures for integrating the spacecraft bus, mission payload and communications payload according to space vehicle level requirements and internal and external ICDs Designs tests to verify the functionality, performance, and safety of the space vehicle, including environmental testing (thermal, vibration, and vacuum tests), performance, and functional testing. Ensures that the integrated space vehicle, test beds, simulators, Electrical Ground Support Equipment (EGSE), and Mechanical Ground Support Equipment (MGSE) meets all technical requirements and specifications through rigorous verification and validation processes. Coordinates interfaces between spacecraft bus, mission payload and communications payload, electrical, software, and mechanical interfaces. Identifies and resolves technical issues and anomalies that arise during integration and testing, working closely with cross-functional teams to address any discrepancies Generates comprehensive documentation, test reports, and data analysis to communicate the results of integration and testing activities Identifies potential risks and develops mitigation strategies to ensure the successful integration and testing of the space vehicle Extracts test and environmental requirements from mission-level and CONOPs and cascades them to all levels of space vehicle testing, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures test functional and physical changes and requirements compliance are being addressed throughout the SV design. Maintains cognizance and communicates changes of the SV subcontractor and in-house test programs Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Electrical Systems Engineers to own and oversees End-to-End integration and test of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle integration and test systems engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads failure review boards, engineering review boards, change control boards to ensure mechanical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS 25% travel as required Ability to lead diverse technical teams across internal and subcontractor efforts Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Mechanical Engineering, Electrical Engineering, Software Engineering, Aerospace Engineering, Systems Engineering, or adjacent field. Active TS/SCI clearance. Experience with integration and test of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience interacting with both internal and external supplier integration and test engineering teams. Experience with integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional test interface details such as EGSE/MGSE designs, test software, test instrumentation, command and data handling, communication, and power paths Experienced with space vehicle, test bed/simulators, EGSE, and MGSE requirements validation, sell-off, milestone entry/exit criteria Familiarity with Digital Engineering and MBSE tools such as CAD, DOORs, CAMEO, CREO, JIRA Ability to make risk-based decisions balancing technical, cost and schedule Ability to support Space Vehicle level electrical, mechanical, and software analyses and trades Strong track record of leading integration and test engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
05/20/2024
Full time
Job Title: Space Vehicle Integration and Test Systems Engineer (Active TS/SCI Clearance Required) Job Code: 10692 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Integration and Test systems engineer (I&T SE) to join our growing team. The individual in this role will act as the primary integration and test systems engineer responsible for coordinating and overseeing verification and test planning for the integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The I&T SE has overall technical responsibility for the design and development of the test plan and flow for the Space Vehicle as well as ownership of the Test Bed and Simulators. The I&T SE serves as the primary point of contact between the SV Engineering team and the Assembly, Integration, and Test (AIT) execution and operations team and coordinates major integration and test activities. The I&T SE will coordinate all integration and test technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Develops, manages and maintains the verification and test plans and procedures for integrating the spacecraft bus, mission payload and communications payload according to space vehicle level requirements and internal and external ICDs Designs tests to verify the functionality, performance, and safety of the space vehicle, including environmental testing (thermal, vibration, and vacuum tests), performance, and functional testing. Ensures that the integrated space vehicle, test beds, simulators, Electrical Ground Support Equipment (EGSE), and Mechanical Ground Support Equipment (MGSE) meets all technical requirements and specifications through rigorous verification and validation processes. Coordinates interfaces between spacecraft bus, mission payload and communications payload, electrical, software, and mechanical interfaces. Identifies and resolves technical issues and anomalies that arise during integration and testing, working closely with cross-functional teams to address any discrepancies Generates comprehensive documentation, test reports, and data analysis to communicate the results of integration and testing activities Identifies potential risks and develops mitigation strategies to ensure the successful integration and testing of the space vehicle Extracts test and environmental requirements from mission-level and CONOPs and cascades them to all levels of space vehicle testing, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures test functional and physical changes and requirements compliance are being addressed throughout the SV design. Maintains cognizance and communicates changes of the SV subcontractor and in-house test programs Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Electrical Systems Engineers to own and oversees End-to-End integration and test of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle integration and test systems engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads failure review boards, engineering review boards, change control boards to ensure mechanical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS 25% travel as required Ability to lead diverse technical teams across internal and subcontractor efforts Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Mechanical Engineering, Electrical Engineering, Software Engineering, Aerospace Engineering, Systems Engineering, or adjacent field. Active TS/SCI clearance. Experience with integration and test of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience interacting with both internal and external supplier integration and test engineering teams. Experience with integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional test interface details such as EGSE/MGSE designs, test software, test instrumentation, command and data handling, communication, and power paths Experienced with space vehicle, test bed/simulators, EGSE, and MGSE requirements validation, sell-off, milestone entry/exit criteria Familiarity with Digital Engineering and MBSE tools such as CAD, DOORs, CAMEO, CREO, JIRA Ability to make risk-based decisions balancing technical, cost and schedule Ability to support Space Vehicle level electrical, mechanical, and software analyses and trades Strong track record of leading integration and test engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
Job Title: Space Vehicle Electrical Systems Engineer (Active TS/SCI Security Clearance Required) Job Code: 10697 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Electrical Systems Engineer (ESE) to join our growing team. The individual in this role will act as the primary electrical systems engineer responsible for mechanical integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The ESE has overall technical responsibility for the electrical design, development, integration, and test for the Space Vehicle and serves as the primary software point of contact for external segments, test, and operations. The ESE will coordinate and/or perform test and analysis integration activities to ensure the system meets Customer and Mission requirements. The ESE will coordinate all electrical technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Manages and maintains the electrical integration of the spacecraft bus, mission payload and communications payload according to internal and external ICDs Generation and coordination of electrical design specifications and interface (internal and external) documents including requirements derivation, allocation, and flow up/down, and V&V activities Extracts mechanical and environmental requirements from mission-level and CONOPs, and cascades them to the spacecraft bus, mission payload, and communications payload, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures electrical functional and physical allocations, changes and requirements compliance are being addressed throughout the SV design. Coordinates and/or completes electrical integration activities such as power and link budgets, channelization, grounding schemes, telemetry and command allocations, and GNC analyses Supports the SEIT organization in planning the electrical integration testing of HW/SW from the subsystem level to the SV level, including execution of SV level tests and troubleshooting issues Maintains cognizance and communicates changes of the SV subcontractor and in-house electrical design baselines, pinouts, and interfaces Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Integration and Test Systems Engineers to own and oversees End-to-End integration of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle electrical engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads or participates in failure review boards, engineering review boards, change control boards to ensure electrical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS Ability to lead diverse technical teams across internal and subcontractor efforts 25% travel as required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Electrical Engineering, Systems Engineering, or adjacent field. Active TS/SCI security clearance. Experience with electrical integration of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience with leading both internal and external supplier electrical engineering teams. Experience with electrical integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional electrical interface details such as first order circuit compatibility, voltage levels, current ratings, connector types, pin configurations, grounding requirements, signal protocols, data rates, communications interfaces and EMI/EMC/ESD considerations Experienced with electrical requirements validation, sell-off, milestone entry/exit criteria Experienced with software integration planning when there are multiple SW/HW solutions in the loop, including flight and test harnesses Experience with writing Statement of Works for external and internal suppliers Familiarity with electrical engineering processes and/or subsystems, such as power, guidance, navigation, and control (GNC), timing, frequency, and ephemeris (TF&E), command and data handling (C&DH), telemetry, tracking, and command (TT&C) Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of leading electrical engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Ability to make risk-based decisions balancing technical, cost and schedule Ability to perform or coordinate Space Vehicle level electrical analyses and trades such channelization, power and link budgets, power systems analysis, electrical loads analysis, fault analysis, electromagnetic compatibility, and worst-case analyses Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
05/20/2024
Full time
Job Title: Space Vehicle Electrical Systems Engineer (Active TS/SCI Security Clearance Required) Job Code: 10697 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Electrical Systems Engineer (ESE) to join our growing team. The individual in this role will act as the primary electrical systems engineer responsible for mechanical integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The ESE has overall technical responsibility for the electrical design, development, integration, and test for the Space Vehicle and serves as the primary software point of contact for external segments, test, and operations. The ESE will coordinate and/or perform test and analysis integration activities to ensure the system meets Customer and Mission requirements. The ESE will coordinate all electrical technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Manages and maintains the electrical integration of the spacecraft bus, mission payload and communications payload according to internal and external ICDs Generation and coordination of electrical design specifications and interface (internal and external) documents including requirements derivation, allocation, and flow up/down, and V&V activities Extracts mechanical and environmental requirements from mission-level and CONOPs, and cascades them to the spacecraft bus, mission payload, and communications payload, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures electrical functional and physical allocations, changes and requirements compliance are being addressed throughout the SV design. Coordinates and/or completes electrical integration activities such as power and link budgets, channelization, grounding schemes, telemetry and command allocations, and GNC analyses Supports the SEIT organization in planning the electrical integration testing of HW/SW from the subsystem level to the SV level, including execution of SV level tests and troubleshooting issues Maintains cognizance and communicates changes of the SV subcontractor and in-house electrical design baselines, pinouts, and interfaces Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Integration and Test Systems Engineers to own and oversees End-to-End integration of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle electrical engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads or participates in failure review boards, engineering review boards, change control boards to ensure electrical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS Ability to lead diverse technical teams across internal and subcontractor efforts 25% travel as required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Electrical Engineering, Systems Engineering, or adjacent field. Active TS/SCI security clearance. Experience with electrical integration of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience with leading both internal and external supplier electrical engineering teams. Experience with electrical integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional electrical interface details such as first order circuit compatibility, voltage levels, current ratings, connector types, pin configurations, grounding requirements, signal protocols, data rates, communications interfaces and EMI/EMC/ESD considerations Experienced with electrical requirements validation, sell-off, milestone entry/exit criteria Experienced with software integration planning when there are multiple SW/HW solutions in the loop, including flight and test harnesses Experience with writing Statement of Works for external and internal suppliers Familiarity with electrical engineering processes and/or subsystems, such as power, guidance, navigation, and control (GNC), timing, frequency, and ephemeris (TF&E), command and data handling (C&DH), telemetry, tracking, and command (TT&C) Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of leading electrical engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Ability to make risk-based decisions balancing technical, cost and schedule Ability to perform or coordinate Space Vehicle level electrical analyses and trades such channelization, power and link budgets, power systems analysis, electrical loads analysis, fault analysis, electromagnetic compatibility, and worst-case analyses Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
Job Title: Space Vehicle Electrical Systems Engineer (Active TS/SCI Security Clearance Required) Job Code: 10697 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Electrical Systems Engineer (ESE) to join our growing team. The individual in this role will act as the primary electrical systems engineer responsible for mechanical integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The ESE has overall technical responsibility for the electrical design, development, integration, and test for the Space Vehicle and serves as the primary software point of contact for external segments, test, and operations. The ESE will coordinate and/or perform test and analysis integration activities to ensure the system meets Customer and Mission requirements. The ESE will coordinate all electrical technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Manages and maintains the electrical integration of the spacecraft bus, mission payload and communications payload according to internal and external ICDs Generation and coordination of electrical design specifications and interface (internal and external) documents including requirements derivation, allocation, and flow up/down, and V&V activities Extracts mechanical and environmental requirements from mission-level and CONOPs, and cascades them to the spacecraft bus, mission payload, and communications payload, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures electrical functional and physical allocations, changes and requirements compliance are being addressed throughout the SV design. Coordinates and/or completes electrical integration activities such as power and link budgets, channelization, grounding schemes, telemetry and command allocations, and GNC analyses Supports the SEIT organization in planning the electrical integration testing of HW/SW from the subsystem level to the SV level, including execution of SV level tests and troubleshooting issues Maintains cognizance and communicates changes of the SV subcontractor and in-house electrical design baselines, pinouts, and interfaces Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Integration and Test Systems Engineers to own and oversees End-to-End integration of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle electrical engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads or participates in failure review boards, engineering review boards, change control boards to ensure electrical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS Ability to lead diverse technical teams across internal and subcontractor efforts 25% travel as required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Electrical Engineering, Systems Engineering, or adjacent field. Active TS/SCI security clearance. Experience with electrical integration of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience with leading both internal and external supplier electrical engineering teams. Experience with electrical integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional electrical interface details such as first order circuit compatibility, voltage levels, current ratings, connector types, pin configurations, grounding requirements, signal protocols, data rates, communications interfaces and EMI/EMC/ESD considerations Experienced with electrical requirements validation, sell-off, milestone entry/exit criteria Experienced with software integration planning when there are multiple SW/HW solutions in the loop, including flight and test harnesses Experience with writing Statement of Works for external and internal suppliers Familiarity with electrical engineering processes and/or subsystems, such as power, guidance, navigation, and control (GNC), timing, frequency, and ephemeris (TF&E), command and data handling (C&DH), telemetry, tracking, and command (TT&C) Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of leading electrical engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Ability to make risk-based decisions balancing technical, cost and schedule Ability to perform or coordinate Space Vehicle level electrical analyses and trades such channelization, power and link budgets, power systems analysis, electrical loads analysis, fault analysis, electromagnetic compatibility, and worst-case analyses Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
05/20/2024
Full time
Job Title: Space Vehicle Electrical Systems Engineer (Active TS/SCI Security Clearance Required) Job Code: 10697 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Electrical Systems Engineer (ESE) to join our growing team. The individual in this role will act as the primary electrical systems engineer responsible for mechanical integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The ESE has overall technical responsibility for the electrical design, development, integration, and test for the Space Vehicle and serves as the primary software point of contact for external segments, test, and operations. The ESE will coordinate and/or perform test and analysis integration activities to ensure the system meets Customer and Mission requirements. The ESE will coordinate all electrical technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Manages and maintains the electrical integration of the spacecraft bus, mission payload and communications payload according to internal and external ICDs Generation and coordination of electrical design specifications and interface (internal and external) documents including requirements derivation, allocation, and flow up/down, and V&V activities Extracts mechanical and environmental requirements from mission-level and CONOPs, and cascades them to the spacecraft bus, mission payload, and communications payload, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures electrical functional and physical allocations, changes and requirements compliance are being addressed throughout the SV design. Coordinates and/or completes electrical integration activities such as power and link budgets, channelization, grounding schemes, telemetry and command allocations, and GNC analyses Supports the SEIT organization in planning the electrical integration testing of HW/SW from the subsystem level to the SV level, including execution of SV level tests and troubleshooting issues Maintains cognizance and communicates changes of the SV subcontractor and in-house electrical design baselines, pinouts, and interfaces Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Integration and Test Systems Engineers to own and oversees End-to-End integration of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle electrical engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads or participates in failure review boards, engineering review boards, change control boards to ensure electrical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS Ability to lead diverse technical teams across internal and subcontractor efforts 25% travel as required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Electrical Engineering, Systems Engineering, or adjacent field. Active TS/SCI security clearance. Experience with electrical integration of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience with leading both internal and external supplier electrical engineering teams. Experience with electrical integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional electrical interface details such as first order circuit compatibility, voltage levels, current ratings, connector types, pin configurations, grounding requirements, signal protocols, data rates, communications interfaces and EMI/EMC/ESD considerations Experienced with electrical requirements validation, sell-off, milestone entry/exit criteria Experienced with software integration planning when there are multiple SW/HW solutions in the loop, including flight and test harnesses Experience with writing Statement of Works for external and internal suppliers Familiarity with electrical engineering processes and/or subsystems, such as power, guidance, navigation, and control (GNC), timing, frequency, and ephemeris (TF&E), command and data handling (C&DH), telemetry, tracking, and command (TT&C) Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of leading electrical engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Ability to make risk-based decisions balancing technical, cost and schedule Ability to perform or coordinate Space Vehicle level electrical analyses and trades such channelization, power and link budgets, power systems analysis, electrical loads analysis, fault analysis, electromagnetic compatibility, and worst-case analyses Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
Job Title: Space Vehicle Electrical Systems Engineer (Active TS/SCI Security Clearance Required) Job Code: 10697 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Electrical Systems Engineer (ESE) to join our growing team. The individual in this role will act as the primary electrical systems engineer responsible for mechanical integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The ESE has overall technical responsibility for the electrical design, development, integration, and test for the Space Vehicle and serves as the primary software point of contact for external segments, test, and operations. The ESE will coordinate and/or perform test and analysis integration activities to ensure the system meets Customer and Mission requirements. The ESE will coordinate all electrical technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Manages and maintains the electrical integration of the spacecraft bus, mission payload and communications payload according to internal and external ICDs Generation and coordination of electrical design specifications and interface (internal and external) documents including requirements derivation, allocation, and flow up/down, and V&V activities Extracts mechanical and environmental requirements from mission-level and CONOPs, and cascades them to the spacecraft bus, mission payload, and communications payload, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures electrical functional and physical allocations, changes and requirements compliance are being addressed throughout the SV design. Coordinates and/or completes electrical integration activities such as power and link budgets, channelization, grounding schemes, telemetry and command allocations, and GNC analyses Supports the SEIT organization in planning the electrical integration testing of HW/SW from the subsystem level to the SV level, including execution of SV level tests and troubleshooting issues Maintains cognizance and communicates changes of the SV subcontractor and in-house electrical design baselines, pinouts, and interfaces Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Integration and Test Systems Engineers to own and oversees End-to-End integration of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle electrical engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads or participates in failure review boards, engineering review boards, change control boards to ensure electrical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS Ability to lead diverse technical teams across internal and subcontractor efforts 25% travel as required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Electrical Engineering, Systems Engineering, or adjacent field. Active TS/SCI security clearance. Experience with electrical integration of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience with leading both internal and external supplier electrical engineering teams. Experience with electrical integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional electrical interface details such as first order circuit compatibility, voltage levels, current ratings, connector types, pin configurations, grounding requirements, signal protocols, data rates, communications interfaces and EMI/EMC/ESD considerations Experienced with electrical requirements validation, sell-off, milestone entry/exit criteria Experienced with software integration planning when there are multiple SW/HW solutions in the loop, including flight and test harnesses Experience with writing Statement of Works for external and internal suppliers Familiarity with electrical engineering processes and/or subsystems, such as power, guidance, navigation, and control (GNC), timing, frequency, and ephemeris (TF&E), command and data handling (C&DH), telemetry, tracking, and command (TT&C) Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of leading electrical engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Ability to make risk-based decisions balancing technical, cost and schedule Ability to perform or coordinate Space Vehicle level electrical analyses and trades such channelization, power and link budgets, power systems analysis, electrical loads analysis, fault analysis, electromagnetic compatibility, and worst-case analyses Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
05/20/2024
Full time
Job Title: Space Vehicle Electrical Systems Engineer (Active TS/SCI Security Clearance Required) Job Code: 10697 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Electrical Systems Engineer (ESE) to join our growing team. The individual in this role will act as the primary electrical systems engineer responsible for mechanical integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The ESE has overall technical responsibility for the electrical design, development, integration, and test for the Space Vehicle and serves as the primary software point of contact for external segments, test, and operations. The ESE will coordinate and/or perform test and analysis integration activities to ensure the system meets Customer and Mission requirements. The ESE will coordinate all electrical technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Manages and maintains the electrical integration of the spacecraft bus, mission payload and communications payload according to internal and external ICDs Generation and coordination of electrical design specifications and interface (internal and external) documents including requirements derivation, allocation, and flow up/down, and V&V activities Extracts mechanical and environmental requirements from mission-level and CONOPs, and cascades them to the spacecraft bus, mission payload, and communications payload, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures electrical functional and physical allocations, changes and requirements compliance are being addressed throughout the SV design. Coordinates and/or completes electrical integration activities such as power and link budgets, channelization, grounding schemes, telemetry and command allocations, and GNC analyses Supports the SEIT organization in planning the electrical integration testing of HW/SW from the subsystem level to the SV level, including execution of SV level tests and troubleshooting issues Maintains cognizance and communicates changes of the SV subcontractor and in-house electrical design baselines, pinouts, and interfaces Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Integration and Test Systems Engineers to own and oversees End-to-End integration of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle electrical engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads or participates in failure review boards, engineering review boards, change control boards to ensure electrical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS Ability to lead diverse technical teams across internal and subcontractor efforts 25% travel as required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Electrical Engineering, Systems Engineering, or adjacent field. Active TS/SCI security clearance. Experience with electrical integration of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience with leading both internal and external supplier electrical engineering teams. Experience with electrical integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional electrical interface details such as first order circuit compatibility, voltage levels, current ratings, connector types, pin configurations, grounding requirements, signal protocols, data rates, communications interfaces and EMI/EMC/ESD considerations Experienced with electrical requirements validation, sell-off, milestone entry/exit criteria Experienced with software integration planning when there are multiple SW/HW solutions in the loop, including flight and test harnesses Experience with writing Statement of Works for external and internal suppliers Familiarity with electrical engineering processes and/or subsystems, such as power, guidance, navigation, and control (GNC), timing, frequency, and ephemeris (TF&E), command and data handling (C&DH), telemetry, tracking, and command (TT&C) Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of leading electrical engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Ability to make risk-based decisions balancing technical, cost and schedule Ability to perform or coordinate Space Vehicle level electrical analyses and trades such channelization, power and link budgets, power systems analysis, electrical loads analysis, fault analysis, electromagnetic compatibility, and worst-case analyses Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
Job Title: Space Vehicle Integration and Test Systems Engineer (Active TS/SCI Clearance Required) Job Code: 10692 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Integration and Test systems engineer (I&T SE) to join our growing team. The individual in this role will act as the primary integration and test systems engineer responsible for coordinating and overseeing verification and test planning for the integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The I&T SE has overall technical responsibility for the design and development of the test plan and flow for the Space Vehicle as well as ownership of the Test Bed and Simulators. The I&T SE serves as the primary point of contact between the SV Engineering team and the Assembly, Integration, and Test (AIT) execution and operations team and coordinates major integration and test activities. The I&T SE will coordinate all integration and test technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Develops, manages and maintains the verification and test plans and procedures for integrating the spacecraft bus, mission payload and communications payload according to space vehicle level requirements and internal and external ICDs Designs tests to verify the functionality, performance, and safety of the space vehicle, including environmental testing (thermal, vibration, and vacuum tests), performance, and functional testing. Ensures that the integrated space vehicle, test beds, simulators, Electrical Ground Support Equipment (EGSE), and Mechanical Ground Support Equipment (MGSE) meets all technical requirements and specifications through rigorous verification and validation processes. Coordinates interfaces between spacecraft bus, mission payload and communications payload, electrical, software, and mechanical interfaces. Identifies and resolves technical issues and anomalies that arise during integration and testing, working closely with cross-functional teams to address any discrepancies Generates comprehensive documentation, test reports, and data analysis to communicate the results of integration and testing activities Identifies potential risks and develops mitigation strategies to ensure the successful integration and testing of the space vehicle Extracts test and environmental requirements from mission-level and CONOPs and cascades them to all levels of space vehicle testing, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures test functional and physical changes and requirements compliance are being addressed throughout the SV design. Maintains cognizance and communicates changes of the SV subcontractor and in-house test programs Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Electrical Systems Engineers to own and oversees End-to-End integration and test of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle integration and test systems engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads failure review boards, engineering review boards, change control boards to ensure mechanical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS 25% travel as required Ability to lead diverse technical teams across internal and subcontractor efforts Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Mechanical Engineering, Electrical Engineering, Software Engineering, Aerospace Engineering, Systems Engineering, or adjacent field. Active TS/SCI clearance. Experience with integration and test of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience interacting with both internal and external supplier integration and test engineering teams. Experience with integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional test interface details such as EGSE/MGSE designs, test software, test instrumentation, command and data handling, communication, and power paths Experienced with space vehicle, test bed/simulators, EGSE, and MGSE requirements validation, sell-off, milestone entry/exit criteria Familiarity with Digital Engineering and MBSE tools such as CAD, DOORs, CAMEO, CREO, JIRA Ability to make risk-based decisions balancing technical, cost and schedule Ability to support Space Vehicle level electrical, mechanical, and software analyses and trades Strong track record of leading integration and test engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
05/20/2024
Full time
Job Title: Space Vehicle Integration and Test Systems Engineer (Active TS/SCI Clearance Required) Job Code: 10692 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Integration and Test systems engineer (I&T SE) to join our growing team. The individual in this role will act as the primary integration and test systems engineer responsible for coordinating and overseeing verification and test planning for the integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The I&T SE has overall technical responsibility for the design and development of the test plan and flow for the Space Vehicle as well as ownership of the Test Bed and Simulators. The I&T SE serves as the primary point of contact between the SV Engineering team and the Assembly, Integration, and Test (AIT) execution and operations team and coordinates major integration and test activities. The I&T SE will coordinate all integration and test technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Develops, manages and maintains the verification and test plans and procedures for integrating the spacecraft bus, mission payload and communications payload according to space vehicle level requirements and internal and external ICDs Designs tests to verify the functionality, performance, and safety of the space vehicle, including environmental testing (thermal, vibration, and vacuum tests), performance, and functional testing. Ensures that the integrated space vehicle, test beds, simulators, Electrical Ground Support Equipment (EGSE), and Mechanical Ground Support Equipment (MGSE) meets all technical requirements and specifications through rigorous verification and validation processes. Coordinates interfaces between spacecraft bus, mission payload and communications payload, electrical, software, and mechanical interfaces. Identifies and resolves technical issues and anomalies that arise during integration and testing, working closely with cross-functional teams to address any discrepancies Generates comprehensive documentation, test reports, and data analysis to communicate the results of integration and testing activities Identifies potential risks and develops mitigation strategies to ensure the successful integration and testing of the space vehicle Extracts test and environmental requirements from mission-level and CONOPs and cascades them to all levels of space vehicle testing, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures test functional and physical changes and requirements compliance are being addressed throughout the SV design. Maintains cognizance and communicates changes of the SV subcontractor and in-house test programs Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Electrical Systems Engineers to own and oversees End-to-End integration and test of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle integration and test systems engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads failure review boards, engineering review boards, change control boards to ensure mechanical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS 25% travel as required Ability to lead diverse technical teams across internal and subcontractor efforts Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Mechanical Engineering, Electrical Engineering, Software Engineering, Aerospace Engineering, Systems Engineering, or adjacent field. Active TS/SCI clearance. Experience with integration and test of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience interacting with both internal and external supplier integration and test engineering teams. Experience with integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional test interface details such as EGSE/MGSE designs, test software, test instrumentation, command and data handling, communication, and power paths Experienced with space vehicle, test bed/simulators, EGSE, and MGSE requirements validation, sell-off, milestone entry/exit criteria Familiarity with Digital Engineering and MBSE tools such as CAD, DOORs, CAMEO, CREO, JIRA Ability to make risk-based decisions balancing technical, cost and schedule Ability to support Space Vehicle level electrical, mechanical, and software analyses and trades Strong track record of leading integration and test engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
Job Title: Lead, Project Systems Engineer Job Location: Salt Lake City, UT Job Code: 10546 Job Schedule: 9/80, every other Friday off Job Description: The Systems Engineer will act as the Project Engineer for the Army ACC ($887M) ID/IQ Program. The system engineer will be the primary technical point of contact for the customer (INSCOM, CECOM, PEO IEW&S) and will lead regular status meeting with the customer as well as provide monthly status reports. The System Engineer will provide program oversight for all technical issues and will work closely with Program Management in administrative functions including engineering budgets, staffing, schedules, and technical risks/opportunities management. This System Engineer will provide technical oversight for the Ground, Aerial, and SATCOM Data Links related work including proposals, development, analysis, system integration & test, product improvement, sustainment, field support, and repairs. The System Engineer must be well versed in all technical aspects of the program. Essential Functions: Provides technical oversight of program engineering team and primary technical point of contract for customer Ensures technical performance, quality, and adherence to established policies and processes Develops and presents project/program reviews for both internal and external customer audiences Leads or assists in project/program schedule and budget planning, subcontract control, risk management Leads or assists in management over systems engineering team and other teams of functional design engineers Ensures technical performance, quality, and adherence to schedule Follows processes in conformance with established policies and objectives Coordinates the efforts of technical support personnel Required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior project systems engineering experience. Preferred Qualifications: US DoD Security Clearance: TS SCI (preferred) Minimum of 7 years' experience with engineering design concepts and engineering practices and procedures required to develop, test and deploy systems. Experience in product development a plus (preferably in military application environment). Presentation and communication skills (verbal/written/visual) Problem solving skills and the ability to meet critical schedule milestones Understanding in coordination of project(s) and efforts of technical support personnel Ability to productively contribute work, ideas and collaboration as part of a team Ability, willingness to travel when required to support customer installation, demonstrations and general field support Proficient in MS Office Suite (Word, Excel, PowerPoint, Project, Visio) Link Budet analysis (Link Budget Software) Earned Value Management System (EVMS) Interconnect Design: Mentor Graphics Capital Logic and/or Visio Requirement Management: IBM Rational DOORS
05/20/2024
Full time
Job Title: Lead, Project Systems Engineer Job Location: Salt Lake City, UT Job Code: 10546 Job Schedule: 9/80, every other Friday off Job Description: The Systems Engineer will act as the Project Engineer for the Army ACC ($887M) ID/IQ Program. The system engineer will be the primary technical point of contact for the customer (INSCOM, CECOM, PEO IEW&S) and will lead regular status meeting with the customer as well as provide monthly status reports. The System Engineer will provide program oversight for all technical issues and will work closely with Program Management in administrative functions including engineering budgets, staffing, schedules, and technical risks/opportunities management. This System Engineer will provide technical oversight for the Ground, Aerial, and SATCOM Data Links related work including proposals, development, analysis, system integration & test, product improvement, sustainment, field support, and repairs. The System Engineer must be well versed in all technical aspects of the program. Essential Functions: Provides technical oversight of program engineering team and primary technical point of contract for customer Ensures technical performance, quality, and adherence to established policies and processes Develops and presents project/program reviews for both internal and external customer audiences Leads or assists in project/program schedule and budget planning, subcontract control, risk management Leads or assists in management over systems engineering team and other teams of functional design engineers Ensures technical performance, quality, and adherence to schedule Follows processes in conformance with established policies and objectives Coordinates the efforts of technical support personnel Required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior project systems engineering experience. Preferred Qualifications: US DoD Security Clearance: TS SCI (preferred) Minimum of 7 years' experience with engineering design concepts and engineering practices and procedures required to develop, test and deploy systems. Experience in product development a plus (preferably in military application environment). Presentation and communication skills (verbal/written/visual) Problem solving skills and the ability to meet critical schedule milestones Understanding in coordination of project(s) and efforts of technical support personnel Ability to productively contribute work, ideas and collaboration as part of a team Ability, willingness to travel when required to support customer installation, demonstrations and general field support Proficient in MS Office Suite (Word, Excel, PowerPoint, Project, Visio) Link Budet analysis (Link Budget Software) Earned Value Management System (EVMS) Interconnect Design: Mentor Graphics Capital Logic and/or Visio Requirement Management: IBM Rational DOORS
Job Title: Lead, Project Systems Engineer Job Location: Salt Lake City, UT Job Code: 10546 Job Schedule: 9/80, every other Friday off Job Description: The Systems Engineer will act as the Project Engineer for the Army ACC ($887M) ID/IQ Program. The system engineer will be the primary technical point of contact for the customer (INSCOM, CECOM, PEO IEW&S) and will lead regular status meeting with the customer as well as provide monthly status reports. The System Engineer will provide program oversight for all technical issues and will work closely with Program Management in administrative functions including engineering budgets, staffing, schedules, and technical risks/opportunities management. This System Engineer will provide technical oversight for the Ground, Aerial, and SATCOM Data Links related work including proposals, development, analysis, system integration & test, product improvement, sustainment, field support, and repairs. The System Engineer must be well versed in all technical aspects of the program. Essential Functions: Provides technical oversight of program engineering team and primary technical point of contract for customer Ensures technical performance, quality, and adherence to established policies and processes Develops and presents project/program reviews for both internal and external customer audiences Leads or assists in project/program schedule and budget planning, subcontract control, risk management Leads or assists in management over systems engineering team and other teams of functional design engineers Ensures technical performance, quality, and adherence to schedule Follows processes in conformance with established policies and objectives Coordinates the efforts of technical support personnel Required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior project systems engineering experience. Preferred Qualifications: US DoD Security Clearance: TS SCI (preferred) Minimum of 7 years' experience with engineering design concepts and engineering practices and procedures required to develop, test and deploy systems. Experience in product development a plus (preferably in military application environment). Presentation and communication skills (verbal/written/visual) Problem solving skills and the ability to meet critical schedule milestones Understanding in coordination of project(s) and efforts of technical support personnel Ability to productively contribute work, ideas and collaboration as part of a team Ability, willingness to travel when required to support customer installation, demonstrations and general field support Proficient in MS Office Suite (Word, Excel, PowerPoint, Project, Visio) Link Budet analysis (Link Budget Software) Earned Value Management System (EVMS) Interconnect Design: Mentor Graphics Capital Logic and/or Visio Requirement Management: IBM Rational DOORS
05/20/2024
Full time
Job Title: Lead, Project Systems Engineer Job Location: Salt Lake City, UT Job Code: 10546 Job Schedule: 9/80, every other Friday off Job Description: The Systems Engineer will act as the Project Engineer for the Army ACC ($887M) ID/IQ Program. The system engineer will be the primary technical point of contact for the customer (INSCOM, CECOM, PEO IEW&S) and will lead regular status meeting with the customer as well as provide monthly status reports. The System Engineer will provide program oversight for all technical issues and will work closely with Program Management in administrative functions including engineering budgets, staffing, schedules, and technical risks/opportunities management. This System Engineer will provide technical oversight for the Ground, Aerial, and SATCOM Data Links related work including proposals, development, analysis, system integration & test, product improvement, sustainment, field support, and repairs. The System Engineer must be well versed in all technical aspects of the program. Essential Functions: Provides technical oversight of program engineering team and primary technical point of contract for customer Ensures technical performance, quality, and adherence to established policies and processes Develops and presents project/program reviews for both internal and external customer audiences Leads or assists in project/program schedule and budget planning, subcontract control, risk management Leads or assists in management over systems engineering team and other teams of functional design engineers Ensures technical performance, quality, and adherence to schedule Follows processes in conformance with established policies and objectives Coordinates the efforts of technical support personnel Required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior project systems engineering experience. Preferred Qualifications: US DoD Security Clearance: TS SCI (preferred) Minimum of 7 years' experience with engineering design concepts and engineering practices and procedures required to develop, test and deploy systems. Experience in product development a plus (preferably in military application environment). Presentation and communication skills (verbal/written/visual) Problem solving skills and the ability to meet critical schedule milestones Understanding in coordination of project(s) and efforts of technical support personnel Ability to productively contribute work, ideas and collaboration as part of a team Ability, willingness to travel when required to support customer installation, demonstrations and general field support Proficient in MS Office Suite (Word, Excel, PowerPoint, Project, Visio) Link Budet analysis (Link Budget Software) Earned Value Management System (EVMS) Interconnect Design: Mentor Graphics Capital Logic and/or Visio Requirement Management: IBM Rational DOORS
Job Title: Space Vehicle Electrical Systems Engineer (Active TS/SCI Security Clearance Required) Job Code: 10697 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Electrical Systems Engineer (ESE) to join our growing team. The individual in this role will act as the primary electrical systems engineer responsible for mechanical integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The ESE has overall technical responsibility for the electrical design, development, integration, and test for the Space Vehicle and serves as the primary software point of contact for external segments, test, and operations. The ESE will coordinate and/or perform test and analysis integration activities to ensure the system meets Customer and Mission requirements. The ESE will coordinate all electrical technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Manages and maintains the electrical integration of the spacecraft bus, mission payload and communications payload according to internal and external ICDs Generation and coordination of electrical design specifications and interface (internal and external) documents including requirements derivation, allocation, and flow up/down, and V&V activities Extracts mechanical and environmental requirements from mission-level and CONOPs, and cascades them to the spacecraft bus, mission payload, and communications payload, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures electrical functional and physical allocations, changes and requirements compliance are being addressed throughout the SV design. Coordinates and/or completes electrical integration activities such as power and link budgets, channelization, grounding schemes, telemetry and command allocations, and GNC analyses Supports the SEIT organization in planning the electrical integration testing of HW/SW from the subsystem level to the SV level, including execution of SV level tests and troubleshooting issues Maintains cognizance and communicates changes of the SV subcontractor and in-house electrical design baselines, pinouts, and interfaces Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Integration and Test Systems Engineers to own and oversees End-to-End integration of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle electrical engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads or participates in failure review boards, engineering review boards, change control boards to ensure electrical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS Ability to lead diverse technical teams across internal and subcontractor efforts 25% travel as required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Electrical Engineering, Systems Engineering, or adjacent field. Active TS/SCI security clearance. Experience with electrical integration of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience with leading both internal and external supplier electrical engineering teams. Experience with electrical integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional electrical interface details such as first order circuit compatibility, voltage levels, current ratings, connector types, pin configurations, grounding requirements, signal protocols, data rates, communications interfaces and EMI/EMC/ESD considerations Experienced with electrical requirements validation, sell-off, milestone entry/exit criteria Experienced with software integration planning when there are multiple SW/HW solutions in the loop, including flight and test harnesses Experience with writing Statement of Works for external and internal suppliers Familiarity with electrical engineering processes and/or subsystems, such as power, guidance, navigation, and control (GNC), timing, frequency, and ephemeris (TF&E), command and data handling (C&DH), telemetry, tracking, and command (TT&C) Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of leading electrical engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Ability to make risk-based decisions balancing technical, cost and schedule Ability to perform or coordinate Space Vehicle level electrical analyses and trades such channelization, power and link budgets, power systems analysis, electrical loads analysis, fault analysis, electromagnetic compatibility, and worst-case analyses Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
05/20/2024
Full time
Job Title: Space Vehicle Electrical Systems Engineer (Active TS/SCI Security Clearance Required) Job Code: 10697 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Electrical Systems Engineer (ESE) to join our growing team. The individual in this role will act as the primary electrical systems engineer responsible for mechanical integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The ESE has overall technical responsibility for the electrical design, development, integration, and test for the Space Vehicle and serves as the primary software point of contact for external segments, test, and operations. The ESE will coordinate and/or perform test and analysis integration activities to ensure the system meets Customer and Mission requirements. The ESE will coordinate all electrical technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Manages and maintains the electrical integration of the spacecraft bus, mission payload and communications payload according to internal and external ICDs Generation and coordination of electrical design specifications and interface (internal and external) documents including requirements derivation, allocation, and flow up/down, and V&V activities Extracts mechanical and environmental requirements from mission-level and CONOPs, and cascades them to the spacecraft bus, mission payload, and communications payload, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures electrical functional and physical allocations, changes and requirements compliance are being addressed throughout the SV design. Coordinates and/or completes electrical integration activities such as power and link budgets, channelization, grounding schemes, telemetry and command allocations, and GNC analyses Supports the SEIT organization in planning the electrical integration testing of HW/SW from the subsystem level to the SV level, including execution of SV level tests and troubleshooting issues Maintains cognizance and communicates changes of the SV subcontractor and in-house electrical design baselines, pinouts, and interfaces Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Integration and Test Systems Engineers to own and oversees End-to-End integration of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle electrical engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads or participates in failure review boards, engineering review boards, change control boards to ensure electrical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS Ability to lead diverse technical teams across internal and subcontractor efforts 25% travel as required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Electrical Engineering, Systems Engineering, or adjacent field. Active TS/SCI security clearance. Experience with electrical integration of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience with leading both internal and external supplier electrical engineering teams. Experience with electrical integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional electrical interface details such as first order circuit compatibility, voltage levels, current ratings, connector types, pin configurations, grounding requirements, signal protocols, data rates, communications interfaces and EMI/EMC/ESD considerations Experienced with electrical requirements validation, sell-off, milestone entry/exit criteria Experienced with software integration planning when there are multiple SW/HW solutions in the loop, including flight and test harnesses Experience with writing Statement of Works for external and internal suppliers Familiarity with electrical engineering processes and/or subsystems, such as power, guidance, navigation, and control (GNC), timing, frequency, and ephemeris (TF&E), command and data handling (C&DH), telemetry, tracking, and command (TT&C) Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of leading electrical engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Ability to make risk-based decisions balancing technical, cost and schedule Ability to perform or coordinate Space Vehicle level electrical analyses and trades such channelization, power and link budgets, power systems analysis, electrical loads analysis, fault analysis, electromagnetic compatibility, and worst-case analyses Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
Job Title: Enterprise Space Vehicle Power Systems Engineer (Active TS/SCI Clearance Required) Job Code: 10698 Job Location: Remote or Palm Bay, FL or Rochester, NY or Fort Wayne, IN or San Diego, CA or Colorado Springs, CO Job Description: L3Harris' Space and Airborne Systems seeks an Enterprise Space Vehicle (SV) Power Engineer to join our growing team. The individual in this position will be serve as an Enterprise SV Power Lead across the Space Sector at L3Harris, responsible for the technical strategy, execution and mentoring of SV Power and Electrical Engineers. This includes all phases of the program lifecycle: Capture and Proposal, Program Execution and Operations. The Enterprise SV Power Lead will be responsible for leading teams of SV level power and electrical engineers through the product life cycle activities ranging from initial requirements and architectures, design and development, integration and test and operations. The role will include occasional direct support to Programs and Customers to ensure execution activities of all functional disciplines for existing portfolio programs and new pursuits. Essential Functions: Establish and standardize SV level Power engineering activities for all phases of the program life cycle Develop processes for standardizing SV level requirements derivation and flow down Develop guidelines for SV level trade studies, common analyses and integration activities tailorable for each mission area and program Review program SV level power engineering work products for consistency Support major technical reviews and failure investigations as an Independent Reviewer Mentor and train program SV level Power Engineers Hold monthly working group meetings across program SV level power engineer to share lessons learned, best practices, ongoing concerns/issues, and potential opportunities Ensure engineering excellence on executing programs through consistent and repeatable SV level power engineering activities across the Sector 25% travel as required Qualifications: Bachelor's Degree with a minimum of 15 years of prior related experience. Graduate Degree with a minimum of 13 years of prior related experience. In lieu of a degree, minimum of 19 years of prior related experience. Active TS/SCI security clearance. High level of prior experience in following areas: Space Vehicle power performance analysis such as processor and memory utilization, data sizing and flows, etc. Integrated Space Vehicle Power CSCIs for end-to-end mission performance Internal and external power interface management Space vehicle fault management architectures and design Leading both internal and external supplier power engineering teams Power/Firmware integration with hardware, testing, and troubleshooting Preferred Additional Skills: Test bed and simulator design process Well versed in fleshing out physical and functional interface details such as data formats and power protocols Familiarity with SW engineering processes such as Agile/Waterfall, DevSecOps, Cont Integration as well as SW development related to embedded/RT/architecture patterns Well versed in functions, responsibilities and interconnectivities between SV SW, Ground SW, Test SW and Operations SW Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of executing all phases of space vehicle programs (SRR, PDR, CDR, TRR, PSR, operations, etc.) System-level requirements verification including allocation, flow down, analysis, testing, & demonstration Ability to make risk-based decisions balancing technical, cost and schedule Familiarity with ConOp development Accustomed to leading technical engagement with internal and external customers in formal presentations as well as informal table-top discussions Excellent communication and presentation skills and the ability to work harmoniously in a team environment with government customers and other contractors Proven analytical and troubleshooting skills demonstrated by related work experience Strong coordination and organization skills with a focus on details Strong track record of leading power engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $153,500 - $285,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
05/20/2024
Full time
Job Title: Enterprise Space Vehicle Power Systems Engineer (Active TS/SCI Clearance Required) Job Code: 10698 Job Location: Remote or Palm Bay, FL or Rochester, NY or Fort Wayne, IN or San Diego, CA or Colorado Springs, CO Job Description: L3Harris' Space and Airborne Systems seeks an Enterprise Space Vehicle (SV) Power Engineer to join our growing team. The individual in this position will be serve as an Enterprise SV Power Lead across the Space Sector at L3Harris, responsible for the technical strategy, execution and mentoring of SV Power and Electrical Engineers. This includes all phases of the program lifecycle: Capture and Proposal, Program Execution and Operations. The Enterprise SV Power Lead will be responsible for leading teams of SV level power and electrical engineers through the product life cycle activities ranging from initial requirements and architectures, design and development, integration and test and operations. The role will include occasional direct support to Programs and Customers to ensure execution activities of all functional disciplines for existing portfolio programs and new pursuits. Essential Functions: Establish and standardize SV level Power engineering activities for all phases of the program life cycle Develop processes for standardizing SV level requirements derivation and flow down Develop guidelines for SV level trade studies, common analyses and integration activities tailorable for each mission area and program Review program SV level power engineering work products for consistency Support major technical reviews and failure investigations as an Independent Reviewer Mentor and train program SV level Power Engineers Hold monthly working group meetings across program SV level power engineer to share lessons learned, best practices, ongoing concerns/issues, and potential opportunities Ensure engineering excellence on executing programs through consistent and repeatable SV level power engineering activities across the Sector 25% travel as required Qualifications: Bachelor's Degree with a minimum of 15 years of prior related experience. Graduate Degree with a minimum of 13 years of prior related experience. In lieu of a degree, minimum of 19 years of prior related experience. Active TS/SCI security clearance. High level of prior experience in following areas: Space Vehicle power performance analysis such as processor and memory utilization, data sizing and flows, etc. Integrated Space Vehicle Power CSCIs for end-to-end mission performance Internal and external power interface management Space vehicle fault management architectures and design Leading both internal and external supplier power engineering teams Power/Firmware integration with hardware, testing, and troubleshooting Preferred Additional Skills: Test bed and simulator design process Well versed in fleshing out physical and functional interface details such as data formats and power protocols Familiarity with SW engineering processes such as Agile/Waterfall, DevSecOps, Cont Integration as well as SW development related to embedded/RT/architecture patterns Well versed in functions, responsibilities and interconnectivities between SV SW, Ground SW, Test SW and Operations SW Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of executing all phases of space vehicle programs (SRR, PDR, CDR, TRR, PSR, operations, etc.) System-level requirements verification including allocation, flow down, analysis, testing, & demonstration Ability to make risk-based decisions balancing technical, cost and schedule Familiarity with ConOp development Accustomed to leading technical engagement with internal and external customers in formal presentations as well as informal table-top discussions Excellent communication and presentation skills and the ability to work harmoniously in a team environment with government customers and other contractors Proven analytical and troubleshooting skills demonstrated by related work experience Strong coordination and organization skills with a focus on details Strong track record of leading power engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $153,500 - $285,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
Schedule: Monday- Friday in Williston, ND The Planning and Scheduling Lead (PL) is a specialist in project schedule development, control and forecasting. The PL assess Contractor and company generated schedules for usefulness, logic, level of detail, input sources, timing, lines of communication, and interfaces with other functional elements and consistency with Current Control Estimate, Work Breakdown Structure (WBS), and the Project Plan The PL also establishes the schedule requirements and frequencies of issue for all of the contractor schedule deliverables. The PL strives for timely detection of trends and specifically deviations from the plan. SKILLS AND QUALIFICATIONS â Bachelors of Science Degree in Engineering, Engineering Technology or Construction Management â Prior oil and gas industry experience preferred â Experience in Project Controls, Project Services and/or Planning/Scheduling â Supervisory experience required â Willing to work overseas in a team environment, relocate to project site as required â Strong influencing, consulting, mentoring, analytical, and computing skills â Advanced competency in Primavera Project Planner (P6) â Adaptability to changing priorities â Excellent interpersonal and communication skills â Ability to multitask and respond quickly to urgent analysis requests With over 90 years' combined experience, NES Fircroft (NES) is proud to be the world's leading engineering staffing provider spanning the Oil & Gas, Power & Renewables, Chemicals, Construction & Infrastructure, Life Sciences, Mining and Manufacturing sectors worldwide. With more than 80 offices in 45 countries, we are able to provide our clients with the engineering and technical expertise they need, wherever and whenever it is needed. We offer contractors far more than a traditional recruitment service, supporting with everything from securing visas and work permits, to providing market-leading benefits packages and accommodation, ensuring they are safely and compliantly able to support our clients.
05/20/2024
Contractor
Schedule: Monday- Friday in Williston, ND The Planning and Scheduling Lead (PL) is a specialist in project schedule development, control and forecasting. The PL assess Contractor and company generated schedules for usefulness, logic, level of detail, input sources, timing, lines of communication, and interfaces with other functional elements and consistency with Current Control Estimate, Work Breakdown Structure (WBS), and the Project Plan The PL also establishes the schedule requirements and frequencies of issue for all of the contractor schedule deliverables. The PL strives for timely detection of trends and specifically deviations from the plan. SKILLS AND QUALIFICATIONS â Bachelors of Science Degree in Engineering, Engineering Technology or Construction Management â Prior oil and gas industry experience preferred â Experience in Project Controls, Project Services and/or Planning/Scheduling â Supervisory experience required â Willing to work overseas in a team environment, relocate to project site as required â Strong influencing, consulting, mentoring, analytical, and computing skills â Advanced competency in Primavera Project Planner (P6) â Adaptability to changing priorities â Excellent interpersonal and communication skills â Ability to multitask and respond quickly to urgent analysis requests With over 90 years' combined experience, NES Fircroft (NES) is proud to be the world's leading engineering staffing provider spanning the Oil & Gas, Power & Renewables, Chemicals, Construction & Infrastructure, Life Sciences, Mining and Manufacturing sectors worldwide. With more than 80 offices in 45 countries, we are able to provide our clients with the engineering and technical expertise they need, wherever and whenever it is needed. We offer contractors far more than a traditional recruitment service, supporting with everything from securing visas and work permits, to providing market-leading benefits packages and accommodation, ensuring they are safely and compliantly able to support our clients.
LifePoint Health Support Center
Brentwood, Tennessee
Manager, Construction Who we are: At Lifepoint Health, we provide quality healthcare to rural communities. As a valued member of our team, you will be an integral part of a group working together to elevate Lifepoint's healthcare delivery network. Our network includes 60+ community hospitals, 60+ rehabilitation/behavioral health hospitals, and 250 additional sites of care across the United States. As an organization, we are dedicated to serving communities nationwide by providing exceptional care. We believe in the power of our talented teams and strive to create environments where employees find purpose and fulfillment. What you'll do: As a Manager, Construction, you will be responsible for assisting with management of construction projects relative to Lifepoint Health's capital development program. Typical construction projects range in cost from $500,000 to in excess of $100 million. Responsibilities: Assist with the following tasks during Pre-Design: o Work with Hospital Administration teams to define the project program. o Develop budgets and constructability analysis. o Prepare required documentation to facilitate CON submittals. o Conduct site investigations to assist with the design and construction oversight and coordination. o Assist with the selection of architects, engineers and contractors. o Assist with the development of design and construction agreement. Assist with the following tasks during Design: o Assist with review and analysis of estimated costs relative to the approved project budget and scope. o Help verify that the established program of the project can be achieved within the approved budget. o Participate in coordination meetings with all internal and external team members. Monitor the design team's schedule and quality control process. o Assist with review of the design documents and vendor drawings to help ensure accuracy, completeness and thorough coordination. o Meet with state and local authorities having jurisdiction over the project to represent Lifepoint and the hospital's interests regarding project scope, design issues and code issues. Assist with the following tasks during Construction: o Analyze contractor cost estimates and bids. Help assess risks relative to subcontractor pricing, schedules, and bonding requirements. o Process contracts and invoices from architects, engineers and contractors, and verify invoices are consistent with the contract terms. Review all proposed changes to ensure charges are legitimate, accurate and appropriate for the work being performed. Monitor project costs against final approved budget. o Visit construction sites routinely at times appropriate for the scope and complexity of the project. o Observe construction activity to verify conformance with the contract documents and quality of workmanship. Identify and document any deficiencies. o Observe contractor's field management personnel to verify the project is being properly and efficiently managed. o Monitor the contractor's scheduling activities to verify a timely completion. o Maintain relations with and manage expectations of hospital administration. Evaluate their requests for changes in design/construction. Communicate progress of construction. o Log progress and action items needed by the design and construction team. Prepare written documentation of issues and directives. o Represent Lifepoint and the hospital at state and local inspections of projects, as necessary. Assist the contractor and architect with responses to inspection issues and review comments. o Assist with developing phasing plans, interim life safety measures, and infection control risk assessments, and help ensure they are followed in order to provide for safety of the public, staff and patient. Assist with the following miscellaneous tasks: o Maintain financials record and reports identifying all costs associated with the project design and construction. Process any necessary changes to the capital requests with the appropriate description and justification. o Utilize architects and engineers on as-needed basis for additional design or construction services during the construction phase. o Perform miscellaneous duties as assigned. o Assist with the management of projects with capital budgets typically greater than $500,000. o As requested, assist with management of projects with capital budgets less than $500,000. What you'll need: EDUCATION: Bachelor's degree in construction management, engineering or architecture preferred. EXPERIENCE: 3+ years of design and construction related experience. Knowledge of healthcare facility engineering, design and construction. Strong interpersonal skills. Effective communication skills for interface with all levels of company management, vendors, contractors, and architects. Strong management and organizational skills to maintain control of activities of numerous projects. Candidate must be able to travel to work locations and construction projects which may have varying degrees of physical accessibility. Working knowledge of pertinent codes and regulations including JCAHO, ADA, OSHA and NFPA. Why choose us: As a team member of the Health Support Center, our goal is to support those that are in our facilities who are interfacing and providing care to our patients and community members. Our focus is to attract, retain, and empower a diverse and determined workforce. Our mission statement is at the heart of who we are and what we do: "Making Communities Healthier." In this shared mission, we believe that our collective efforts will shape a healthier future for the communities we serve. Benefits: We offer an excellent total compensation package, including a competitive salary and benefits. Some of our benefits include 401k, flexible PTO, generous Employee illness benefit (EIB), medical, dental, vision, tuition reimbursement, and an Employee Assistance Program. We believe that happy, healthy people have a passionate engagement with life and work and have designed our package to enhance your wellbeing. Equal opportunity and affirmative action employers and are looking for diversity in candidates for employment: Minority/Female/Disabled/Protected Veteran
05/20/2024
Full time
Manager, Construction Who we are: At Lifepoint Health, we provide quality healthcare to rural communities. As a valued member of our team, you will be an integral part of a group working together to elevate Lifepoint's healthcare delivery network. Our network includes 60+ community hospitals, 60+ rehabilitation/behavioral health hospitals, and 250 additional sites of care across the United States. As an organization, we are dedicated to serving communities nationwide by providing exceptional care. We believe in the power of our talented teams and strive to create environments where employees find purpose and fulfillment. What you'll do: As a Manager, Construction, you will be responsible for assisting with management of construction projects relative to Lifepoint Health's capital development program. Typical construction projects range in cost from $500,000 to in excess of $100 million. Responsibilities: Assist with the following tasks during Pre-Design: o Work with Hospital Administration teams to define the project program. o Develop budgets and constructability analysis. o Prepare required documentation to facilitate CON submittals. o Conduct site investigations to assist with the design and construction oversight and coordination. o Assist with the selection of architects, engineers and contractors. o Assist with the development of design and construction agreement. Assist with the following tasks during Design: o Assist with review and analysis of estimated costs relative to the approved project budget and scope. o Help verify that the established program of the project can be achieved within the approved budget. o Participate in coordination meetings with all internal and external team members. Monitor the design team's schedule and quality control process. o Assist with review of the design documents and vendor drawings to help ensure accuracy, completeness and thorough coordination. o Meet with state and local authorities having jurisdiction over the project to represent Lifepoint and the hospital's interests regarding project scope, design issues and code issues. Assist with the following tasks during Construction: o Analyze contractor cost estimates and bids. Help assess risks relative to subcontractor pricing, schedules, and bonding requirements. o Process contracts and invoices from architects, engineers and contractors, and verify invoices are consistent with the contract terms. Review all proposed changes to ensure charges are legitimate, accurate and appropriate for the work being performed. Monitor project costs against final approved budget. o Visit construction sites routinely at times appropriate for the scope and complexity of the project. o Observe construction activity to verify conformance with the contract documents and quality of workmanship. Identify and document any deficiencies. o Observe contractor's field management personnel to verify the project is being properly and efficiently managed. o Monitor the contractor's scheduling activities to verify a timely completion. o Maintain relations with and manage expectations of hospital administration. Evaluate their requests for changes in design/construction. Communicate progress of construction. o Log progress and action items needed by the design and construction team. Prepare written documentation of issues and directives. o Represent Lifepoint and the hospital at state and local inspections of projects, as necessary. Assist the contractor and architect with responses to inspection issues and review comments. o Assist with developing phasing plans, interim life safety measures, and infection control risk assessments, and help ensure they are followed in order to provide for safety of the public, staff and patient. Assist with the following miscellaneous tasks: o Maintain financials record and reports identifying all costs associated with the project design and construction. Process any necessary changes to the capital requests with the appropriate description and justification. o Utilize architects and engineers on as-needed basis for additional design or construction services during the construction phase. o Perform miscellaneous duties as assigned. o Assist with the management of projects with capital budgets typically greater than $500,000. o As requested, assist with management of projects with capital budgets less than $500,000. What you'll need: EDUCATION: Bachelor's degree in construction management, engineering or architecture preferred. EXPERIENCE: 3+ years of design and construction related experience. Knowledge of healthcare facility engineering, design and construction. Strong interpersonal skills. Effective communication skills for interface with all levels of company management, vendors, contractors, and architects. Strong management and organizational skills to maintain control of activities of numerous projects. Candidate must be able to travel to work locations and construction projects which may have varying degrees of physical accessibility. Working knowledge of pertinent codes and regulations including JCAHO, ADA, OSHA and NFPA. Why choose us: As a team member of the Health Support Center, our goal is to support those that are in our facilities who are interfacing and providing care to our patients and community members. Our focus is to attract, retain, and empower a diverse and determined workforce. Our mission statement is at the heart of who we are and what we do: "Making Communities Healthier." In this shared mission, we believe that our collective efforts will shape a healthier future for the communities we serve. Benefits: We offer an excellent total compensation package, including a competitive salary and benefits. Some of our benefits include 401k, flexible PTO, generous Employee illness benefit (EIB), medical, dental, vision, tuition reimbursement, and an Employee Assistance Program. We believe that happy, healthy people have a passionate engagement with life and work and have designed our package to enhance your wellbeing. Equal opportunity and affirmative action employers and are looking for diversity in candidates for employment: Minority/Female/Disabled/Protected Veteran
Metallurgic Process Engineering Manager Our client is looking for a Metal/Forging Process Engineering Manager for their heavy industry operation in the greater Ogden, UT area. Experience Requirements: BS degree in Mechanical Engineering (Metallurgical, Material Science & Nuclear may be acceptable) 10+ years of professional experience in Industrial Manufacturing. Metallurgy experience and management of technical team of engineers is a plus. Working knowledge of manufacturing equipment, techniques, processes and procedures. Experience in project estimating and project management. Computer literate; proficiency in word processing, spreadsheets, knowledge of Wonderware Historian database. Experience in Process Hazard Analysis (PHA) and other Hazard Identification and Risk Analysis tools would be a plus. Skill Competencies Ability to guide Process Engineers in applying broad knowledge of engineering skills, principles, practices, and procedures to complete difficult and complex assignments. Must have strong analytical and problem-solving skills and demonstrated experience. Must have strong time management skills to handle multiple ongoing projects in addition to day-to-day process problems. Solid computer skills including Microsoft Office & PowerPoint, MiniTab, and the ability to quickly learn software such as Leading to Lean, etc. Problem Solving Resolve chemical, metallurgical, and mechanical problems for and with employees, management, customer(s) and /or vendor(s). Act as a liaison with internal and external customers. Act as the liaison between Maintenance and Manufacturing to provide technical support. Use vision and drive to establish the processes and controls necessary to meet the expected growth of the facility. Assess and develop employee skills to troubleshoot and resolve issues effectively Determine appropriate machine and process down-time operations in conjunction with production requirements. Able to define problems, collects data, establish facts, and draw valid conclusions. Knowledge of interpreting a variety of technical instructions in mathematical or diagram form and deal with several abstract and concrete variables. Ability to read, analyze, and interpret general business and financial data, write technical procedures and possesses grammar skills to write reports and business correspondence. Use six sigma, lean or other tools to improve the implementation of manufacturing processes. Develop employees for future career opportunities. Determine ways to recognize and reward employee behavior. Major Responsibilities: Determine and review all Fabrication manufacturing processes for cost effectiveness, feasibility, and customer compliance before and after engineering releases to manufacturing. Determine priorities with the Plant/Department Managers and implement cost-reduction projects; maintain detailed documentation as required. Analyze and design lean manufacturing cells and lines. Help guide designs for DFM (Design for Manufacturing) Direct department activities for design of new products to meet customer specifications, modify existing designs, improve production techniques, and develop test and verification procedures for manufacturing operations. Understand welding systems and operations. Assign departmental personnel to specific manufacturing areas/phases or aspects of project such as technical studies, product design, preparation of specifications and technical plans, and product testing, verification and qualification. Coach employees in career planning activities. Plan and formulate engineering program and organize department staff according to project and/or manufacturing requirements. Work closely with Design Engineering, Operations, Quality Assurance, and Maintenance personnel to prevent problems with products and tooling/fixtures. Maintain integration of the Process Engineers into the EP&T Organization. Provide engineering leadership that aligns with EP&T engineering in terms of project execution, change control, engineering discipline, and integration with appropriate disciplines for project or change execution. Review and monitor all design, engineering, and proposed technological development/enhancement as related to product lines. Manages projects chosen for manufacturing. Ensure reliable product delivery meeting objectives for quality, cost and production according to schedule. Develop and maintains department standard operating procedures, training, manuals, drawing standards, including the development and maintenance of Process Design Basis, Control Requirement Documentation in ENOVIA and Equipment specifications maintained in Leading to Lean database. Review product design for compliance with engineering principles, company standards, and customer contract requirements, and related specifications. Maintain positive relationship with product customers and interface during audit visits. Evaluate and approves design changes, calculations, specifications, and drawing releases. Communicate key metrics for safety, quality, and production to employees to properly align actions and behaviors for improvement. Maintain Process Safety Information on all Safety Significant Process and ensure PHAa are current. Participate and appoint Process Engineers to regularly participated in Process Hazard Analysis as required. Priorities include: Maintain and Improve bench strength of Fabrication Process Engineering in Melting, Round and Flat Product Departments. Develop and maintain Process Design Basis and Control Requirement Documentation for existing systems and equipment for all departments and in ENOVIA database. PSM Improvement Initiatives: Update Fabrication Process Safety Information documentation (PSI) (P&IDs, PDBs, CRDs, Pressure Relief Valves and PMs, Critical Equipment/controls, etc.) and ensure all such information is maintained in Enovia and Leading to Lean (L2L) database. Support Department Shutdowns and Startups and help to fill gaps in missing technical information Review and update procedures that would help improve and maintain more stable operations Modify and update systems to improve overall performance and return the system to its original design basis as needed Engineering projects and assignments Cost Improvement Projects following project management processes and change control Cost of Poor-Quality Monthly reporting and improvement projects Monthly Data input to Accounting for Quarterly Continuous Improvement Meeting Conduct Monthly Fabrication Process/Quality Meeting Support Kaizen and continuous improvement projects for Fabrication departments. Maintain qualification/verification standards and direct efforts to support Supply Chain investigating alternative and new sources for Fabrication raw materials, equipment and instrument parts.
05/20/2024
Metallurgic Process Engineering Manager Our client is looking for a Metal/Forging Process Engineering Manager for their heavy industry operation in the greater Ogden, UT area. Experience Requirements: BS degree in Mechanical Engineering (Metallurgical, Material Science & Nuclear may be acceptable) 10+ years of professional experience in Industrial Manufacturing. Metallurgy experience and management of technical team of engineers is a plus. Working knowledge of manufacturing equipment, techniques, processes and procedures. Experience in project estimating and project management. Computer literate; proficiency in word processing, spreadsheets, knowledge of Wonderware Historian database. Experience in Process Hazard Analysis (PHA) and other Hazard Identification and Risk Analysis tools would be a plus. Skill Competencies Ability to guide Process Engineers in applying broad knowledge of engineering skills, principles, practices, and procedures to complete difficult and complex assignments. Must have strong analytical and problem-solving skills and demonstrated experience. Must have strong time management skills to handle multiple ongoing projects in addition to day-to-day process problems. Solid computer skills including Microsoft Office & PowerPoint, MiniTab, and the ability to quickly learn software such as Leading to Lean, etc. Problem Solving Resolve chemical, metallurgical, and mechanical problems for and with employees, management, customer(s) and /or vendor(s). Act as a liaison with internal and external customers. Act as the liaison between Maintenance and Manufacturing to provide technical support. Use vision and drive to establish the processes and controls necessary to meet the expected growth of the facility. Assess and develop employee skills to troubleshoot and resolve issues effectively Determine appropriate machine and process down-time operations in conjunction with production requirements. Able to define problems, collects data, establish facts, and draw valid conclusions. Knowledge of interpreting a variety of technical instructions in mathematical or diagram form and deal with several abstract and concrete variables. Ability to read, analyze, and interpret general business and financial data, write technical procedures and possesses grammar skills to write reports and business correspondence. Use six sigma, lean or other tools to improve the implementation of manufacturing processes. Develop employees for future career opportunities. Determine ways to recognize and reward employee behavior. Major Responsibilities: Determine and review all Fabrication manufacturing processes for cost effectiveness, feasibility, and customer compliance before and after engineering releases to manufacturing. Determine priorities with the Plant/Department Managers and implement cost-reduction projects; maintain detailed documentation as required. Analyze and design lean manufacturing cells and lines. Help guide designs for DFM (Design for Manufacturing) Direct department activities for design of new products to meet customer specifications, modify existing designs, improve production techniques, and develop test and verification procedures for manufacturing operations. Understand welding systems and operations. Assign departmental personnel to specific manufacturing areas/phases or aspects of project such as technical studies, product design, preparation of specifications and technical plans, and product testing, verification and qualification. Coach employees in career planning activities. Plan and formulate engineering program and organize department staff according to project and/or manufacturing requirements. Work closely with Design Engineering, Operations, Quality Assurance, and Maintenance personnel to prevent problems with products and tooling/fixtures. Maintain integration of the Process Engineers into the EP&T Organization. Provide engineering leadership that aligns with EP&T engineering in terms of project execution, change control, engineering discipline, and integration with appropriate disciplines for project or change execution. Review and monitor all design, engineering, and proposed technological development/enhancement as related to product lines. Manages projects chosen for manufacturing. Ensure reliable product delivery meeting objectives for quality, cost and production according to schedule. Develop and maintains department standard operating procedures, training, manuals, drawing standards, including the development and maintenance of Process Design Basis, Control Requirement Documentation in ENOVIA and Equipment specifications maintained in Leading to Lean database. Review product design for compliance with engineering principles, company standards, and customer contract requirements, and related specifications. Maintain positive relationship with product customers and interface during audit visits. Evaluate and approves design changes, calculations, specifications, and drawing releases. Communicate key metrics for safety, quality, and production to employees to properly align actions and behaviors for improvement. Maintain Process Safety Information on all Safety Significant Process and ensure PHAa are current. Participate and appoint Process Engineers to regularly participated in Process Hazard Analysis as required. Priorities include: Maintain and Improve bench strength of Fabrication Process Engineering in Melting, Round and Flat Product Departments. Develop and maintain Process Design Basis and Control Requirement Documentation for existing systems and equipment for all departments and in ENOVIA database. PSM Improvement Initiatives: Update Fabrication Process Safety Information documentation (PSI) (P&IDs, PDBs, CRDs, Pressure Relief Valves and PMs, Critical Equipment/controls, etc.) and ensure all such information is maintained in Enovia and Leading to Lean (L2L) database. Support Department Shutdowns and Startups and help to fill gaps in missing technical information Review and update procedures that would help improve and maintain more stable operations Modify and update systems to improve overall performance and return the system to its original design basis as needed Engineering projects and assignments Cost Improvement Projects following project management processes and change control Cost of Poor-Quality Monthly reporting and improvement projects Monthly Data input to Accounting for Quarterly Continuous Improvement Meeting Conduct Monthly Fabrication Process/Quality Meeting Support Kaizen and continuous improvement projects for Fabrication departments. Maintain qualification/verification standards and direct efforts to support Supply Chain investigating alternative and new sources for Fabrication raw materials, equipment and instrument parts.
Job Title: Space Vehicle Electrical Systems Engineer (Active TS/SCI Security Clearance Required) Job Code: 10697 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Electrical Systems Engineer (ESE) to join our growing team. The individual in this role will act as the primary electrical systems engineer responsible for mechanical integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The ESE has overall technical responsibility for the electrical design, development, integration, and test for the Space Vehicle and serves as the primary software point of contact for external segments, test, and operations. The ESE will coordinate and/or perform test and analysis integration activities to ensure the system meets Customer and Mission requirements. The ESE will coordinate all electrical technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Manages and maintains the electrical integration of the spacecraft bus, mission payload and communications payload according to internal and external ICDs Generation and coordination of electrical design specifications and interface (internal and external) documents including requirements derivation, allocation, and flow up/down, and V&V activities Extracts mechanical and environmental requirements from mission-level and CONOPs, and cascades them to the spacecraft bus, mission payload, and communications payload, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures electrical functional and physical allocations, changes and requirements compliance are being addressed throughout the SV design. Coordinates and/or completes electrical integration activities such as power and link budgets, channelization, grounding schemes, telemetry and command allocations, and GNC analyses Supports the SEIT organization in planning the electrical integration testing of HW/SW from the subsystem level to the SV level, including execution of SV level tests and troubleshooting issues Maintains cognizance and communicates changes of the SV subcontractor and in-house electrical design baselines, pinouts, and interfaces Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Integration and Test Systems Engineers to own and oversees End-to-End integration of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle electrical engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads or participates in failure review boards, engineering review boards, change control boards to ensure electrical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS Ability to lead diverse technical teams across internal and subcontractor efforts 25% travel as required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Electrical Engineering, Systems Engineering, or adjacent field. Active TS/SCI security clearance. Experience with electrical integration of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience with leading both internal and external supplier electrical engineering teams. Experience with electrical integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional electrical interface details such as first order circuit compatibility, voltage levels, current ratings, connector types, pin configurations, grounding requirements, signal protocols, data rates, communications interfaces and EMI/EMC/ESD considerations Experienced with electrical requirements validation, sell-off, milestone entry/exit criteria Experienced with software integration planning when there are multiple SW/HW solutions in the loop, including flight and test harnesses Experience with writing Statement of Works for external and internal suppliers Familiarity with electrical engineering processes and/or subsystems, such as power, guidance, navigation, and control (GNC), timing, frequency, and ephemeris (TF&E), command and data handling (C&DH), telemetry, tracking, and command (TT&C) Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of leading electrical engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Ability to make risk-based decisions balancing technical, cost and schedule Ability to perform or coordinate Space Vehicle level electrical analyses and trades such channelization, power and link budgets, power systems analysis, electrical loads analysis, fault analysis, electromagnetic compatibility, and worst-case analyses Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
05/20/2024
Full time
Job Title: Space Vehicle Electrical Systems Engineer (Active TS/SCI Security Clearance Required) Job Code: 10697 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Electrical Systems Engineer (ESE) to join our growing team. The individual in this role will act as the primary electrical systems engineer responsible for mechanical integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The ESE has overall technical responsibility for the electrical design, development, integration, and test for the Space Vehicle and serves as the primary software point of contact for external segments, test, and operations. The ESE will coordinate and/or perform test and analysis integration activities to ensure the system meets Customer and Mission requirements. The ESE will coordinate all electrical technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Manages and maintains the electrical integration of the spacecraft bus, mission payload and communications payload according to internal and external ICDs Generation and coordination of electrical design specifications and interface (internal and external) documents including requirements derivation, allocation, and flow up/down, and V&V activities Extracts mechanical and environmental requirements from mission-level and CONOPs, and cascades them to the spacecraft bus, mission payload, and communications payload, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures electrical functional and physical allocations, changes and requirements compliance are being addressed throughout the SV design. Coordinates and/or completes electrical integration activities such as power and link budgets, channelization, grounding schemes, telemetry and command allocations, and GNC analyses Supports the SEIT organization in planning the electrical integration testing of HW/SW from the subsystem level to the SV level, including execution of SV level tests and troubleshooting issues Maintains cognizance and communicates changes of the SV subcontractor and in-house electrical design baselines, pinouts, and interfaces Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Integration and Test Systems Engineers to own and oversees End-to-End integration of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle electrical engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads or participates in failure review boards, engineering review boards, change control boards to ensure electrical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS Ability to lead diverse technical teams across internal and subcontractor efforts 25% travel as required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Electrical Engineering, Systems Engineering, or adjacent field. Active TS/SCI security clearance. Experience with electrical integration of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience with leading both internal and external supplier electrical engineering teams. Experience with electrical integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional electrical interface details such as first order circuit compatibility, voltage levels, current ratings, connector types, pin configurations, grounding requirements, signal protocols, data rates, communications interfaces and EMI/EMC/ESD considerations Experienced with electrical requirements validation, sell-off, milestone entry/exit criteria Experienced with software integration planning when there are multiple SW/HW solutions in the loop, including flight and test harnesses Experience with writing Statement of Works for external and internal suppliers Familiarity with electrical engineering processes and/or subsystems, such as power, guidance, navigation, and control (GNC), timing, frequency, and ephemeris (TF&E), command and data handling (C&DH), telemetry, tracking, and command (TT&C) Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of leading electrical engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Ability to make risk-based decisions balancing technical, cost and schedule Ability to perform or coordinate Space Vehicle level electrical analyses and trades such channelization, power and link budgets, power systems analysis, electrical loads analysis, fault analysis, electromagnetic compatibility, and worst-case analyses Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
Job Title: Enterprise Space Vehicle Power Systems Engineer (Active TS/SCI Clearance Required) Job Code: 10698 Job Location: Remote or Palm Bay, FL or Rochester, NY or Fort Wayne, IN or San Diego, CA or Colorado Springs, CO Job Description: L3Harris' Space and Airborne Systems seeks an Enterprise Space Vehicle (SV) Power Engineer to join our growing team. The individual in this position will be serve as an Enterprise SV Power Lead across the Space Sector at L3Harris, responsible for the technical strategy, execution and mentoring of SV Power and Electrical Engineers. This includes all phases of the program lifecycle: Capture and Proposal, Program Execution and Operations. The Enterprise SV Power Lead will be responsible for leading teams of SV level power and electrical engineers through the product life cycle activities ranging from initial requirements and architectures, design and development, integration and test and operations. The role will include occasional direct support to Programs and Customers to ensure execution activities of all functional disciplines for existing portfolio programs and new pursuits. Essential Functions: Establish and standardize SV level Power engineering activities for all phases of the program life cycle Develop processes for standardizing SV level requirements derivation and flow down Develop guidelines for SV level trade studies, common analyses and integration activities tailorable for each mission area and program Review program SV level power engineering work products for consistency Support major technical reviews and failure investigations as an Independent Reviewer Mentor and train program SV level Power Engineers Hold monthly working group meetings across program SV level power engineer to share lessons learned, best practices, ongoing concerns/issues, and potential opportunities Ensure engineering excellence on executing programs through consistent and repeatable SV level power engineering activities across the Sector 25% travel as required Qualifications: Bachelor's Degree with a minimum of 15 years of prior related experience. Graduate Degree with a minimum of 13 years of prior related experience. In lieu of a degree, minimum of 19 years of prior related experience. Active TS/SCI security clearance. High level of prior experience in following areas: Space Vehicle power performance analysis such as processor and memory utilization, data sizing and flows, etc. Integrated Space Vehicle Power CSCIs for end-to-end mission performance Internal and external power interface management Space vehicle fault management architectures and design Leading both internal and external supplier power engineering teams Power/Firmware integration with hardware, testing, and troubleshooting Preferred Additional Skills: Test bed and simulator design process Well versed in fleshing out physical and functional interface details such as data formats and power protocols Familiarity with SW engineering processes such as Agile/Waterfall, DevSecOps, Cont Integration as well as SW development related to embedded/RT/architecture patterns Well versed in functions, responsibilities and interconnectivities between SV SW, Ground SW, Test SW and Operations SW Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of executing all phases of space vehicle programs (SRR, PDR, CDR, TRR, PSR, operations, etc.) System-level requirements verification including allocation, flow down, analysis, testing, & demonstration Ability to make risk-based decisions balancing technical, cost and schedule Familiarity with ConOp development Accustomed to leading technical engagement with internal and external customers in formal presentations as well as informal table-top discussions Excellent communication and presentation skills and the ability to work harmoniously in a team environment with government customers and other contractors Proven analytical and troubleshooting skills demonstrated by related work experience Strong coordination and organization skills with a focus on details Strong track record of leading power engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $153,500 - $285,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
05/20/2024
Full time
Job Title: Enterprise Space Vehicle Power Systems Engineer (Active TS/SCI Clearance Required) Job Code: 10698 Job Location: Remote or Palm Bay, FL or Rochester, NY or Fort Wayne, IN or San Diego, CA or Colorado Springs, CO Job Description: L3Harris' Space and Airborne Systems seeks an Enterprise Space Vehicle (SV) Power Engineer to join our growing team. The individual in this position will be serve as an Enterprise SV Power Lead across the Space Sector at L3Harris, responsible for the technical strategy, execution and mentoring of SV Power and Electrical Engineers. This includes all phases of the program lifecycle: Capture and Proposal, Program Execution and Operations. The Enterprise SV Power Lead will be responsible for leading teams of SV level power and electrical engineers through the product life cycle activities ranging from initial requirements and architectures, design and development, integration and test and operations. The role will include occasional direct support to Programs and Customers to ensure execution activities of all functional disciplines for existing portfolio programs and new pursuits. Essential Functions: Establish and standardize SV level Power engineering activities for all phases of the program life cycle Develop processes for standardizing SV level requirements derivation and flow down Develop guidelines for SV level trade studies, common analyses and integration activities tailorable for each mission area and program Review program SV level power engineering work products for consistency Support major technical reviews and failure investigations as an Independent Reviewer Mentor and train program SV level Power Engineers Hold monthly working group meetings across program SV level power engineer to share lessons learned, best practices, ongoing concerns/issues, and potential opportunities Ensure engineering excellence on executing programs through consistent and repeatable SV level power engineering activities across the Sector 25% travel as required Qualifications: Bachelor's Degree with a minimum of 15 years of prior related experience. Graduate Degree with a minimum of 13 years of prior related experience. In lieu of a degree, minimum of 19 years of prior related experience. Active TS/SCI security clearance. High level of prior experience in following areas: Space Vehicle power performance analysis such as processor and memory utilization, data sizing and flows, etc. Integrated Space Vehicle Power CSCIs for end-to-end mission performance Internal and external power interface management Space vehicle fault management architectures and design Leading both internal and external supplier power engineering teams Power/Firmware integration with hardware, testing, and troubleshooting Preferred Additional Skills: Test bed and simulator design process Well versed in fleshing out physical and functional interface details such as data formats and power protocols Familiarity with SW engineering processes such as Agile/Waterfall, DevSecOps, Cont Integration as well as SW development related to embedded/RT/architecture patterns Well versed in functions, responsibilities and interconnectivities between SV SW, Ground SW, Test SW and Operations SW Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of executing all phases of space vehicle programs (SRR, PDR, CDR, TRR, PSR, operations, etc.) System-level requirements verification including allocation, flow down, analysis, testing, & demonstration Ability to make risk-based decisions balancing technical, cost and schedule Familiarity with ConOp development Accustomed to leading technical engagement with internal and external customers in formal presentations as well as informal table-top discussions Excellent communication and presentation skills and the ability to work harmoniously in a team environment with government customers and other contractors Proven analytical and troubleshooting skills demonstrated by related work experience Strong coordination and organization skills with a focus on details Strong track record of leading power engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $153,500 - $285,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
Job Title: Lead, Project Systems Engineer Job Location: Salt Lake City, UT Job Code: 10546 Job Schedule: 9/80, every other Friday off Job Description: The Systems Engineer will act as the Project Engineer for the Army ACC ($887M) ID/IQ Program. The system engineer will be the primary technical point of contact for the customer (INSCOM, CECOM, PEO IEW&S) and will lead regular status meeting with the customer as well as provide monthly status reports. The System Engineer will provide program oversight for all technical issues and will work closely with Program Management in administrative functions including engineering budgets, staffing, schedules, and technical risks/opportunities management. This System Engineer will provide technical oversight for the Ground, Aerial, and SATCOM Data Links related work including proposals, development, analysis, system integration & test, product improvement, sustainment, field support, and repairs. The System Engineer must be well versed in all technical aspects of the program. Essential Functions: Provides technical oversight of program engineering team and primary technical point of contract for customer Ensures technical performance, quality, and adherence to established policies and processes Develops and presents project/program reviews for both internal and external customer audiences Leads or assists in project/program schedule and budget planning, subcontract control, risk management Leads or assists in management over systems engineering team and other teams of functional design engineers Ensures technical performance, quality, and adherence to schedule Follows processes in conformance with established policies and objectives Coordinates the efforts of technical support personnel Required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior project systems engineering experience. Preferred Qualifications: US DoD Security Clearance: TS SCI (preferred) Minimum of 7 years' experience with engineering design concepts and engineering practices and procedures required to develop, test and deploy systems. Experience in product development a plus (preferably in military application environment). Presentation and communication skills (verbal/written/visual) Problem solving skills and the ability to meet critical schedule milestones Understanding in coordination of project(s) and efforts of technical support personnel Ability to productively contribute work, ideas and collaboration as part of a team Ability, willingness to travel when required to support customer installation, demonstrations and general field support Proficient in MS Office Suite (Word, Excel, PowerPoint, Project, Visio) Link Budet analysis (Link Budget Software) Earned Value Management System (EVMS) Interconnect Design: Mentor Graphics Capital Logic and/or Visio Requirement Management: IBM Rational DOORS
05/20/2024
Full time
Job Title: Lead, Project Systems Engineer Job Location: Salt Lake City, UT Job Code: 10546 Job Schedule: 9/80, every other Friday off Job Description: The Systems Engineer will act as the Project Engineer for the Army ACC ($887M) ID/IQ Program. The system engineer will be the primary technical point of contact for the customer (INSCOM, CECOM, PEO IEW&S) and will lead regular status meeting with the customer as well as provide monthly status reports. The System Engineer will provide program oversight for all technical issues and will work closely with Program Management in administrative functions including engineering budgets, staffing, schedules, and technical risks/opportunities management. This System Engineer will provide technical oversight for the Ground, Aerial, and SATCOM Data Links related work including proposals, development, analysis, system integration & test, product improvement, sustainment, field support, and repairs. The System Engineer must be well versed in all technical aspects of the program. Essential Functions: Provides technical oversight of program engineering team and primary technical point of contract for customer Ensures technical performance, quality, and adherence to established policies and processes Develops and presents project/program reviews for both internal and external customer audiences Leads or assists in project/program schedule and budget planning, subcontract control, risk management Leads or assists in management over systems engineering team and other teams of functional design engineers Ensures technical performance, quality, and adherence to schedule Follows processes in conformance with established policies and objectives Coordinates the efforts of technical support personnel Required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior project systems engineering experience. Preferred Qualifications: US DoD Security Clearance: TS SCI (preferred) Minimum of 7 years' experience with engineering design concepts and engineering practices and procedures required to develop, test and deploy systems. Experience in product development a plus (preferably in military application environment). Presentation and communication skills (verbal/written/visual) Problem solving skills and the ability to meet critical schedule milestones Understanding in coordination of project(s) and efforts of technical support personnel Ability to productively contribute work, ideas and collaboration as part of a team Ability, willingness to travel when required to support customer installation, demonstrations and general field support Proficient in MS Office Suite (Word, Excel, PowerPoint, Project, Visio) Link Budet analysis (Link Budget Software) Earned Value Management System (EVMS) Interconnect Design: Mentor Graphics Capital Logic and/or Visio Requirement Management: IBM Rational DOORS
Job Title: Space Vehicle Integration and Test Systems Engineer (Active TS/SCI Clearance Required) Job Code: 10692 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Integration and Test systems engineer (I&T SE) to join our growing team. The individual in this role will act as the primary integration and test systems engineer responsible for coordinating and overseeing verification and test planning for the integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The I&T SE has overall technical responsibility for the design and development of the test plan and flow for the Space Vehicle as well as ownership of the Test Bed and Simulators. The I&T SE serves as the primary point of contact between the SV Engineering team and the Assembly, Integration, and Test (AIT) execution and operations team and coordinates major integration and test activities. The I&T SE will coordinate all integration and test technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Develops, manages and maintains the verification and test plans and procedures for integrating the spacecraft bus, mission payload and communications payload according to space vehicle level requirements and internal and external ICDs Designs tests to verify the functionality, performance, and safety of the space vehicle, including environmental testing (thermal, vibration, and vacuum tests), performance, and functional testing. Ensures that the integrated space vehicle, test beds, simulators, Electrical Ground Support Equipment (EGSE), and Mechanical Ground Support Equipment (MGSE) meets all technical requirements and specifications through rigorous verification and validation processes. Coordinates interfaces between spacecraft bus, mission payload and communications payload, electrical, software, and mechanical interfaces. Identifies and resolves technical issues and anomalies that arise during integration and testing, working closely with cross-functional teams to address any discrepancies Generates comprehensive documentation, test reports, and data analysis to communicate the results of integration and testing activities Identifies potential risks and develops mitigation strategies to ensure the successful integration and testing of the space vehicle Extracts test and environmental requirements from mission-level and CONOPs and cascades them to all levels of space vehicle testing, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures test functional and physical changes and requirements compliance are being addressed throughout the SV design. Maintains cognizance and communicates changes of the SV subcontractor and in-house test programs Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Electrical Systems Engineers to own and oversees End-to-End integration and test of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle integration and test systems engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads failure review boards, engineering review boards, change control boards to ensure mechanical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS 25% travel as required Ability to lead diverse technical teams across internal and subcontractor efforts Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Mechanical Engineering, Electrical Engineering, Software Engineering, Aerospace Engineering, Systems Engineering, or adjacent field. Active TS/SCI clearance. Experience with integration and test of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience interacting with both internal and external supplier integration and test engineering teams. Experience with integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional test interface details such as EGSE/MGSE designs, test software, test instrumentation, command and data handling, communication, and power paths Experienced with space vehicle, test bed/simulators, EGSE, and MGSE requirements validation, sell-off, milestone entry/exit criteria Familiarity with Digital Engineering and MBSE tools such as CAD, DOORs, CAMEO, CREO, JIRA Ability to make risk-based decisions balancing technical, cost and schedule Ability to support Space Vehicle level electrical, mechanical, and software analyses and trades Strong track record of leading integration and test engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
05/20/2024
Full time
Job Title: Space Vehicle Integration and Test Systems Engineer (Active TS/SCI Clearance Required) Job Code: 10692 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Integration and Test systems engineer (I&T SE) to join our growing team. The individual in this role will act as the primary integration and test systems engineer responsible for coordinating and overseeing verification and test planning for the integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The I&T SE has overall technical responsibility for the design and development of the test plan and flow for the Space Vehicle as well as ownership of the Test Bed and Simulators. The I&T SE serves as the primary point of contact between the SV Engineering team and the Assembly, Integration, and Test (AIT) execution and operations team and coordinates major integration and test activities. The I&T SE will coordinate all integration and test technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Develops, manages and maintains the verification and test plans and procedures for integrating the spacecraft bus, mission payload and communications payload according to space vehicle level requirements and internal and external ICDs Designs tests to verify the functionality, performance, and safety of the space vehicle, including environmental testing (thermal, vibration, and vacuum tests), performance, and functional testing. Ensures that the integrated space vehicle, test beds, simulators, Electrical Ground Support Equipment (EGSE), and Mechanical Ground Support Equipment (MGSE) meets all technical requirements and specifications through rigorous verification and validation processes. Coordinates interfaces between spacecraft bus, mission payload and communications payload, electrical, software, and mechanical interfaces. Identifies and resolves technical issues and anomalies that arise during integration and testing, working closely with cross-functional teams to address any discrepancies Generates comprehensive documentation, test reports, and data analysis to communicate the results of integration and testing activities Identifies potential risks and develops mitigation strategies to ensure the successful integration and testing of the space vehicle Extracts test and environmental requirements from mission-level and CONOPs and cascades them to all levels of space vehicle testing, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures test functional and physical changes and requirements compliance are being addressed throughout the SV design. Maintains cognizance and communicates changes of the SV subcontractor and in-house test programs Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Electrical Systems Engineers to own and oversees End-to-End integration and test of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle integration and test systems engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads failure review boards, engineering review boards, change control boards to ensure mechanical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS 25% travel as required Ability to lead diverse technical teams across internal and subcontractor efforts Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Mechanical Engineering, Electrical Engineering, Software Engineering, Aerospace Engineering, Systems Engineering, or adjacent field. Active TS/SCI clearance. Experience with integration and test of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience interacting with both internal and external supplier integration and test engineering teams. Experience with integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional test interface details such as EGSE/MGSE designs, test software, test instrumentation, command and data handling, communication, and power paths Experienced with space vehicle, test bed/simulators, EGSE, and MGSE requirements validation, sell-off, milestone entry/exit criteria Familiarity with Digital Engineering and MBSE tools such as CAD, DOORs, CAMEO, CREO, JIRA Ability to make risk-based decisions balancing technical, cost and schedule Ability to support Space Vehicle level electrical, mechanical, and software analyses and trades Strong track record of leading integration and test engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
Job Title: Space Vehicle Integration and Test Systems Engineer (Active TS/SCI Clearance Required) Job Code: 10692 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Integration and Test systems engineer (I&T SE) to join our growing team. The individual in this role will act as the primary integration and test systems engineer responsible for coordinating and overseeing verification and test planning for the integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The I&T SE has overall technical responsibility for the design and development of the test plan and flow for the Space Vehicle as well as ownership of the Test Bed and Simulators. The I&T SE serves as the primary point of contact between the SV Engineering team and the Assembly, Integration, and Test (AIT) execution and operations team and coordinates major integration and test activities. The I&T SE will coordinate all integration and test technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Develops, manages and maintains the verification and test plans and procedures for integrating the spacecraft bus, mission payload and communications payload according to space vehicle level requirements and internal and external ICDs Designs tests to verify the functionality, performance, and safety of the space vehicle, including environmental testing (thermal, vibration, and vacuum tests), performance, and functional testing. Ensures that the integrated space vehicle, test beds, simulators, Electrical Ground Support Equipment (EGSE), and Mechanical Ground Support Equipment (MGSE) meets all technical requirements and specifications through rigorous verification and validation processes. Coordinates interfaces between spacecraft bus, mission payload and communications payload, electrical, software, and mechanical interfaces. Identifies and resolves technical issues and anomalies that arise during integration and testing, working closely with cross-functional teams to address any discrepancies Generates comprehensive documentation, test reports, and data analysis to communicate the results of integration and testing activities Identifies potential risks and develops mitigation strategies to ensure the successful integration and testing of the space vehicle Extracts test and environmental requirements from mission-level and CONOPs and cascades them to all levels of space vehicle testing, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures test functional and physical changes and requirements compliance are being addressed throughout the SV design. Maintains cognizance and communicates changes of the SV subcontractor and in-house test programs Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Electrical Systems Engineers to own and oversees End-to-End integration and test of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle integration and test systems engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads failure review boards, engineering review boards, change control boards to ensure mechanical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS 25% travel as required Ability to lead diverse technical teams across internal and subcontractor efforts Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Mechanical Engineering, Electrical Engineering, Software Engineering, Aerospace Engineering, Systems Engineering, or adjacent field. Active TS/SCI clearance. Experience with integration and test of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience interacting with both internal and external supplier integration and test engineering teams. Experience with integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional test interface details such as EGSE/MGSE designs, test software, test instrumentation, command and data handling, communication, and power paths Experienced with space vehicle, test bed/simulators, EGSE, and MGSE requirements validation, sell-off, milestone entry/exit criteria Familiarity with Digital Engineering and MBSE tools such as CAD, DOORs, CAMEO, CREO, JIRA Ability to make risk-based decisions balancing technical, cost and schedule Ability to support Space Vehicle level electrical, mechanical, and software analyses and trades Strong track record of leading integration and test engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
05/20/2024
Full time
Job Title: Space Vehicle Integration and Test Systems Engineer (Active TS/SCI Clearance Required) Job Code: 10692 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Integration and Test systems engineer (I&T SE) to join our growing team. The individual in this role will act as the primary integration and test systems engineer responsible for coordinating and overseeing verification and test planning for the integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The I&T SE has overall technical responsibility for the design and development of the test plan and flow for the Space Vehicle as well as ownership of the Test Bed and Simulators. The I&T SE serves as the primary point of contact between the SV Engineering team and the Assembly, Integration, and Test (AIT) execution and operations team and coordinates major integration and test activities. The I&T SE will coordinate all integration and test technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Develops, manages and maintains the verification and test plans and procedures for integrating the spacecraft bus, mission payload and communications payload according to space vehicle level requirements and internal and external ICDs Designs tests to verify the functionality, performance, and safety of the space vehicle, including environmental testing (thermal, vibration, and vacuum tests), performance, and functional testing. Ensures that the integrated space vehicle, test beds, simulators, Electrical Ground Support Equipment (EGSE), and Mechanical Ground Support Equipment (MGSE) meets all technical requirements and specifications through rigorous verification and validation processes. Coordinates interfaces between spacecraft bus, mission payload and communications payload, electrical, software, and mechanical interfaces. Identifies and resolves technical issues and anomalies that arise during integration and testing, working closely with cross-functional teams to address any discrepancies Generates comprehensive documentation, test reports, and data analysis to communicate the results of integration and testing activities Identifies potential risks and develops mitigation strategies to ensure the successful integration and testing of the space vehicle Extracts test and environmental requirements from mission-level and CONOPs and cascades them to all levels of space vehicle testing, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures test functional and physical changes and requirements compliance are being addressed throughout the SV design. Maintains cognizance and communicates changes of the SV subcontractor and in-house test programs Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Electrical Systems Engineers to own and oversees End-to-End integration and test of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle integration and test systems engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads failure review boards, engineering review boards, change control boards to ensure mechanical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS 25% travel as required Ability to lead diverse technical teams across internal and subcontractor efforts Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Mechanical Engineering, Electrical Engineering, Software Engineering, Aerospace Engineering, Systems Engineering, or adjacent field. Active TS/SCI clearance. Experience with integration and test of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience interacting with both internal and external supplier integration and test engineering teams. Experience with integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional test interface details such as EGSE/MGSE designs, test software, test instrumentation, command and data handling, communication, and power paths Experienced with space vehicle, test bed/simulators, EGSE, and MGSE requirements validation, sell-off, milestone entry/exit criteria Familiarity with Digital Engineering and MBSE tools such as CAD, DOORs, CAMEO, CREO, JIRA Ability to make risk-based decisions balancing technical, cost and schedule Ability to support Space Vehicle level electrical, mechanical, and software analyses and trades Strong track record of leading integration and test engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
Job Title: Enterprise Space Vehicle Power Systems Engineer (Active TS/SCI Clearance Required) Job Code: 10698 Job Location: Remote or Palm Bay, FL or Rochester, NY or Fort Wayne, IN or San Diego, CA or Colorado Springs, CO Job Description: L3Harris' Space and Airborne Systems seeks an Enterprise Space Vehicle (SV) Power Engineer to join our growing team. The individual in this position will be serve as an Enterprise SV Power Lead across the Space Sector at L3Harris, responsible for the technical strategy, execution and mentoring of SV Power and Electrical Engineers. This includes all phases of the program lifecycle: Capture and Proposal, Program Execution and Operations. The Enterprise SV Power Lead will be responsible for leading teams of SV level power and electrical engineers through the product life cycle activities ranging from initial requirements and architectures, design and development, integration and test and operations. The role will include occasional direct support to Programs and Customers to ensure execution activities of all functional disciplines for existing portfolio programs and new pursuits. Essential Functions: Establish and standardize SV level Power engineering activities for all phases of the program life cycle Develop processes for standardizing SV level requirements derivation and flow down Develop guidelines for SV level trade studies, common analyses and integration activities tailorable for each mission area and program Review program SV level power engineering work products for consistency Support major technical reviews and failure investigations as an Independent Reviewer Mentor and train program SV level Power Engineers Hold monthly working group meetings across program SV level power engineer to share lessons learned, best practices, ongoing concerns/issues, and potential opportunities Ensure engineering excellence on executing programs through consistent and repeatable SV level power engineering activities across the Sector 25% travel as required Qualifications: Bachelor's Degree with a minimum of 15 years of prior related experience. Graduate Degree with a minimum of 13 years of prior related experience. In lieu of a degree, minimum of 19 years of prior related experience. Active TS/SCI security clearance. High level of prior experience in following areas: Space Vehicle power performance analysis such as processor and memory utilization, data sizing and flows, etc. Integrated Space Vehicle Power CSCIs for end-to-end mission performance Internal and external power interface management Space vehicle fault management architectures and design Leading both internal and external supplier power engineering teams Power/Firmware integration with hardware, testing, and troubleshooting Preferred Additional Skills: Test bed and simulator design process Well versed in fleshing out physical and functional interface details such as data formats and power protocols Familiarity with SW engineering processes such as Agile/Waterfall, DevSecOps, Cont Integration as well as SW development related to embedded/RT/architecture patterns Well versed in functions, responsibilities and interconnectivities between SV SW, Ground SW, Test SW and Operations SW Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of executing all phases of space vehicle programs (SRR, PDR, CDR, TRR, PSR, operations, etc.) System-level requirements verification including allocation, flow down, analysis, testing, & demonstration Ability to make risk-based decisions balancing technical, cost and schedule Familiarity with ConOp development Accustomed to leading technical engagement with internal and external customers in formal presentations as well as informal table-top discussions Excellent communication and presentation skills and the ability to work harmoniously in a team environment with government customers and other contractors Proven analytical and troubleshooting skills demonstrated by related work experience Strong coordination and organization skills with a focus on details Strong track record of leading power engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $153,500 - $285,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
05/20/2024
Full time
Job Title: Enterprise Space Vehicle Power Systems Engineer (Active TS/SCI Clearance Required) Job Code: 10698 Job Location: Remote or Palm Bay, FL or Rochester, NY or Fort Wayne, IN or San Diego, CA or Colorado Springs, CO Job Description: L3Harris' Space and Airborne Systems seeks an Enterprise Space Vehicle (SV) Power Engineer to join our growing team. The individual in this position will be serve as an Enterprise SV Power Lead across the Space Sector at L3Harris, responsible for the technical strategy, execution and mentoring of SV Power and Electrical Engineers. This includes all phases of the program lifecycle: Capture and Proposal, Program Execution and Operations. The Enterprise SV Power Lead will be responsible for leading teams of SV level power and electrical engineers through the product life cycle activities ranging from initial requirements and architectures, design and development, integration and test and operations. The role will include occasional direct support to Programs and Customers to ensure execution activities of all functional disciplines for existing portfolio programs and new pursuits. Essential Functions: Establish and standardize SV level Power engineering activities for all phases of the program life cycle Develop processes for standardizing SV level requirements derivation and flow down Develop guidelines for SV level trade studies, common analyses and integration activities tailorable for each mission area and program Review program SV level power engineering work products for consistency Support major technical reviews and failure investigations as an Independent Reviewer Mentor and train program SV level Power Engineers Hold monthly working group meetings across program SV level power engineer to share lessons learned, best practices, ongoing concerns/issues, and potential opportunities Ensure engineering excellence on executing programs through consistent and repeatable SV level power engineering activities across the Sector 25% travel as required Qualifications: Bachelor's Degree with a minimum of 15 years of prior related experience. Graduate Degree with a minimum of 13 years of prior related experience. In lieu of a degree, minimum of 19 years of prior related experience. Active TS/SCI security clearance. High level of prior experience in following areas: Space Vehicle power performance analysis such as processor and memory utilization, data sizing and flows, etc. Integrated Space Vehicle Power CSCIs for end-to-end mission performance Internal and external power interface management Space vehicle fault management architectures and design Leading both internal and external supplier power engineering teams Power/Firmware integration with hardware, testing, and troubleshooting Preferred Additional Skills: Test bed and simulator design process Well versed in fleshing out physical and functional interface details such as data formats and power protocols Familiarity with SW engineering processes such as Agile/Waterfall, DevSecOps, Cont Integration as well as SW development related to embedded/RT/architecture patterns Well versed in functions, responsibilities and interconnectivities between SV SW, Ground SW, Test SW and Operations SW Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of executing all phases of space vehicle programs (SRR, PDR, CDR, TRR, PSR, operations, etc.) System-level requirements verification including allocation, flow down, analysis, testing, & demonstration Ability to make risk-based decisions balancing technical, cost and schedule Familiarity with ConOp development Accustomed to leading technical engagement with internal and external customers in formal presentations as well as informal table-top discussions Excellent communication and presentation skills and the ability to work harmoniously in a team environment with government customers and other contractors Proven analytical and troubleshooting skills demonstrated by related work experience Strong coordination and organization skills with a focus on details Strong track record of leading power engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $153,500 - $285,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
Job Title: Enterprise Space Vehicle Power Systems Engineer (Active TS/SCI Clearance Required) Job Code: 10698 Job Location: Remote or Palm Bay, FL or Rochester, NY or Fort Wayne, IN or San Diego, CA or Colorado Springs, CO Job Description: L3Harris' Space and Airborne Systems seeks an Enterprise Space Vehicle (SV) Power Engineer to join our growing team. The individual in this position will be serve as an Enterprise SV Power Lead across the Space Sector at L3Harris, responsible for the technical strategy, execution and mentoring of SV Power and Electrical Engineers. This includes all phases of the program lifecycle: Capture and Proposal, Program Execution and Operations. The Enterprise SV Power Lead will be responsible for leading teams of SV level power and electrical engineers through the product life cycle activities ranging from initial requirements and architectures, design and development, integration and test and operations. The role will include occasional direct support to Programs and Customers to ensure execution activities of all functional disciplines for existing portfolio programs and new pursuits. Essential Functions: Establish and standardize SV level Power engineering activities for all phases of the program life cycle Develop processes for standardizing SV level requirements derivation and flow down Develop guidelines for SV level trade studies, common analyses and integration activities tailorable for each mission area and program Review program SV level power engineering work products for consistency Support major technical reviews and failure investigations as an Independent Reviewer Mentor and train program SV level Power Engineers Hold monthly working group meetings across program SV level power engineer to share lessons learned, best practices, ongoing concerns/issues, and potential opportunities Ensure engineering excellence on executing programs through consistent and repeatable SV level power engineering activities across the Sector 25% travel as required Qualifications: Bachelor's Degree with a minimum of 15 years of prior related experience. Graduate Degree with a minimum of 13 years of prior related experience. In lieu of a degree, minimum of 19 years of prior related experience. Active TS/SCI security clearance. High level of prior experience in following areas: Space Vehicle power performance analysis such as processor and memory utilization, data sizing and flows, etc. Integrated Space Vehicle Power CSCIs for end-to-end mission performance Internal and external power interface management Space vehicle fault management architectures and design Leading both internal and external supplier power engineering teams Power/Firmware integration with hardware, testing, and troubleshooting Preferred Additional Skills: Test bed and simulator design process Well versed in fleshing out physical and functional interface details such as data formats and power protocols Familiarity with SW engineering processes such as Agile/Waterfall, DevSecOps, Cont Integration as well as SW development related to embedded/RT/architecture patterns Well versed in functions, responsibilities and interconnectivities between SV SW, Ground SW, Test SW and Operations SW Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of executing all phases of space vehicle programs (SRR, PDR, CDR, TRR, PSR, operations, etc.) System-level requirements verification including allocation, flow down, analysis, testing, & demonstration Ability to make risk-based decisions balancing technical, cost and schedule Familiarity with ConOp development Accustomed to leading technical engagement with internal and external customers in formal presentations as well as informal table-top discussions Excellent communication and presentation skills and the ability to work harmoniously in a team environment with government customers and other contractors Proven analytical and troubleshooting skills demonstrated by related work experience Strong coordination and organization skills with a focus on details Strong track record of leading power engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $153,500 - $285,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
05/20/2024
Full time
Job Title: Enterprise Space Vehicle Power Systems Engineer (Active TS/SCI Clearance Required) Job Code: 10698 Job Location: Remote or Palm Bay, FL or Rochester, NY or Fort Wayne, IN or San Diego, CA or Colorado Springs, CO Job Description: L3Harris' Space and Airborne Systems seeks an Enterprise Space Vehicle (SV) Power Engineer to join our growing team. The individual in this position will be serve as an Enterprise SV Power Lead across the Space Sector at L3Harris, responsible for the technical strategy, execution and mentoring of SV Power and Electrical Engineers. This includes all phases of the program lifecycle: Capture and Proposal, Program Execution and Operations. The Enterprise SV Power Lead will be responsible for leading teams of SV level power and electrical engineers through the product life cycle activities ranging from initial requirements and architectures, design and development, integration and test and operations. The role will include occasional direct support to Programs and Customers to ensure execution activities of all functional disciplines for existing portfolio programs and new pursuits. Essential Functions: Establish and standardize SV level Power engineering activities for all phases of the program life cycle Develop processes for standardizing SV level requirements derivation and flow down Develop guidelines for SV level trade studies, common analyses and integration activities tailorable for each mission area and program Review program SV level power engineering work products for consistency Support major technical reviews and failure investigations as an Independent Reviewer Mentor and train program SV level Power Engineers Hold monthly working group meetings across program SV level power engineer to share lessons learned, best practices, ongoing concerns/issues, and potential opportunities Ensure engineering excellence on executing programs through consistent and repeatable SV level power engineering activities across the Sector 25% travel as required Qualifications: Bachelor's Degree with a minimum of 15 years of prior related experience. Graduate Degree with a minimum of 13 years of prior related experience. In lieu of a degree, minimum of 19 years of prior related experience. Active TS/SCI security clearance. High level of prior experience in following areas: Space Vehicle power performance analysis such as processor and memory utilization, data sizing and flows, etc. Integrated Space Vehicle Power CSCIs for end-to-end mission performance Internal and external power interface management Space vehicle fault management architectures and design Leading both internal and external supplier power engineering teams Power/Firmware integration with hardware, testing, and troubleshooting Preferred Additional Skills: Test bed and simulator design process Well versed in fleshing out physical and functional interface details such as data formats and power protocols Familiarity with SW engineering processes such as Agile/Waterfall, DevSecOps, Cont Integration as well as SW development related to embedded/RT/architecture patterns Well versed in functions, responsibilities and interconnectivities between SV SW, Ground SW, Test SW and Operations SW Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of executing all phases of space vehicle programs (SRR, PDR, CDR, TRR, PSR, operations, etc.) System-level requirements verification including allocation, flow down, analysis, testing, & demonstration Ability to make risk-based decisions balancing technical, cost and schedule Familiarity with ConOp development Accustomed to leading technical engagement with internal and external customers in formal presentations as well as informal table-top discussions Excellent communication and presentation skills and the ability to work harmoniously in a team environment with government customers and other contractors Proven analytical and troubleshooting skills demonstrated by related work experience Strong coordination and organization skills with a focus on details Strong track record of leading power engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $153,500 - $285,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
Job Title: Space Vehicle Electrical Systems Engineer (Active TS/SCI Security Clearance Required) Job Code: 10697 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Electrical Systems Engineer (ESE) to join our growing team. The individual in this role will act as the primary electrical systems engineer responsible for mechanical integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The ESE has overall technical responsibility for the electrical design, development, integration, and test for the Space Vehicle and serves as the primary software point of contact for external segments, test, and operations. The ESE will coordinate and/or perform test and analysis integration activities to ensure the system meets Customer and Mission requirements. The ESE will coordinate all electrical technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Manages and maintains the electrical integration of the spacecraft bus, mission payload and communications payload according to internal and external ICDs Generation and coordination of electrical design specifications and interface (internal and external) documents including requirements derivation, allocation, and flow up/down, and V&V activities Extracts mechanical and environmental requirements from mission-level and CONOPs, and cascades them to the spacecraft bus, mission payload, and communications payload, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures electrical functional and physical allocations, changes and requirements compliance are being addressed throughout the SV design. Coordinates and/or completes electrical integration activities such as power and link budgets, channelization, grounding schemes, telemetry and command allocations, and GNC analyses Supports the SEIT organization in planning the electrical integration testing of HW/SW from the subsystem level to the SV level, including execution of SV level tests and troubleshooting issues Maintains cognizance and communicates changes of the SV subcontractor and in-house electrical design baselines, pinouts, and interfaces Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Integration and Test Systems Engineers to own and oversees End-to-End integration of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle electrical engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads or participates in failure review boards, engineering review boards, change control boards to ensure electrical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS Ability to lead diverse technical teams across internal and subcontractor efforts 25% travel as required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Electrical Engineering, Systems Engineering, or adjacent field. Active TS/SCI security clearance. Experience with electrical integration of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience with leading both internal and external supplier electrical engineering teams. Experience with electrical integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional electrical interface details such as first order circuit compatibility, voltage levels, current ratings, connector types, pin configurations, grounding requirements, signal protocols, data rates, communications interfaces and EMI/EMC/ESD considerations Experienced with electrical requirements validation, sell-off, milestone entry/exit criteria Experienced with software integration planning when there are multiple SW/HW solutions in the loop, including flight and test harnesses Experience with writing Statement of Works for external and internal suppliers Familiarity with electrical engineering processes and/or subsystems, such as power, guidance, navigation, and control (GNC), timing, frequency, and ephemeris (TF&E), command and data handling (C&DH), telemetry, tracking, and command (TT&C) Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of leading electrical engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Ability to make risk-based decisions balancing technical, cost and schedule Ability to perform or coordinate Space Vehicle level electrical analyses and trades such channelization, power and link budgets, power systems analysis, electrical loads analysis, fault analysis, electromagnetic compatibility, and worst-case analyses Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.
05/20/2024
Full time
Job Title: Space Vehicle Electrical Systems Engineer (Active TS/SCI Security Clearance Required) Job Code: 10697 Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CA Job Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Electrical Systems Engineer (ESE) to join our growing team. The individual in this role will act as the primary electrical systems engineer responsible for mechanical integration of the spacecraft bus, mission payload, and communication payload to ensure seamless end-to-end mission performance. The ESE has overall technical responsibility for the electrical design, development, integration, and test for the Space Vehicle and serves as the primary software point of contact for external segments, test, and operations. The ESE will coordinate and/or perform test and analysis integration activities to ensure the system meets Customer and Mission requirements. The ESE will coordinate all electrical technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Manages and maintains the electrical integration of the spacecraft bus, mission payload and communications payload according to internal and external ICDs Generation and coordination of electrical design specifications and interface (internal and external) documents including requirements derivation, allocation, and flow up/down, and V&V activities Extracts mechanical and environmental requirements from mission-level and CONOPs, and cascades them to the spacecraft bus, mission payload, and communications payload, encompassing allocations into software, firmware, and hardware, as well as test beds and simulators. Ensures electrical functional and physical allocations, changes and requirements compliance are being addressed throughout the SV design. Coordinates and/or completes electrical integration activities such as power and link budgets, channelization, grounding schemes, telemetry and command allocations, and GNC analyses Supports the SEIT organization in planning the electrical integration testing of HW/SW from the subsystem level to the SV level, including execution of SV level tests and troubleshooting issues Maintains cognizance and communicates changes of the SV subcontractor and in-house electrical design baselines, pinouts, and interfaces Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generation Works closely with Software, Mechanical, and Integration and Test Systems Engineers to own and oversees End-to-End integration of spacecraft bus, mission payload, and communications payload across the full program lifecycle Represent Space Vehicle electrical engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDR Leads or participates in failure review boards, engineering review boards, change control boards to ensure electrical impacts are coordinated across the SV Creating and/or supporting delivery of Customer CDRLS Ability to lead diverse technical teams across internal and subcontractor efforts 25% travel as required Qualifications: Bachelor's Degree and minimum 9 years of prior relevant experience. Graduate Degree and a minimum of 7 years of prior related experience. In lieu of a degree, minimum of 13 years of prior related experience. Bachelor's Degree in Electrical Engineering, Systems Engineering, or adjacent field. Active TS/SCI security clearance. Experience with electrical integration of spacecraft busses, mission payloads, and communications payloads for seamless end-to-end mission performance. Experience with leading both internal and external supplier electrical engineering teams. Experience with electrical integration, testing, and troubleshooting of complex systems. Preferred Additional Skills: Well versed in fleshing out or coordinating physical and functional electrical interface details such as first order circuit compatibility, voltage levels, current ratings, connector types, pin configurations, grounding requirements, signal protocols, data rates, communications interfaces and EMI/EMC/ESD considerations Experienced with electrical requirements validation, sell-off, milestone entry/exit criteria Experienced with software integration planning when there are multiple SW/HW solutions in the loop, including flight and test harnesses Experience with writing Statement of Works for external and internal suppliers Familiarity with electrical engineering processes and/or subsystems, such as power, guidance, navigation, and control (GNC), timing, frequency, and ephemeris (TF&E), command and data handling (C&DH), telemetry, tracking, and command (TT&C) Familiarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRA Strong track record of leading electrical engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operations Ability to make risk-based decisions balancing technical, cost and schedule Ability to perform or coordinate Space Vehicle level electrical analyses and trades such channelization, power and link budgets, power systems analysis, electrical loads analysis, fault analysis, electromagnetic compatibility, and worst-case analyses Experience in mentoring and growing technical staff In compliance with pay transparency requirements, the salary range for this role is $106,500 - $197,500. This is not a guarantee of compensation or salary, as final offer amount may vary based on factors including but not limited to experience and geographic location. L3Harris also offers a variety of benefits, including health and disability insurance, 401(k) match, flexible spending accounts, EAP, education assistance, parental leave, paid time off, and company-paid holidays. The specific programs and options available to an employee may vary depending on date of hire, schedule type, and the applicability of collective bargaining agreements. The application window for this requisition is anticipated to close July 31, 2024.