Firmware Engineer Salary in Indiana, USA

Job Title: Enterprise Space Vehicle Software Systems Engineer (Active TS/SCI Clearance Required)Job Code: 10701Job Location: Remote or Palm Bay, FL or Rochester, NY or Fort Wayne, IN or San Diego, CA or Colorado Springs, COJob Description:L3Harris' Space and Airborne Systems seeks an Enterprise Space Vehicle (SV) Software Engineer to join our growing team. The individual in this position will be serve as an Enterprise SV Software Engineer Lead across the Space Sector at L3Harris, responsible for the technical strategy, execution and mentoring of SV Software Engineers. This includes all phases of the program lifecycle: Capture and Proposal, Program Execution and Operations. The Enterprise SV Software Engineer will be responsible for leading teams of SV software 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 Software engineering activities for all phases of the program life cycleDevelop processes for standardizing SV level software requirements derivation and flow down Develop guidelines for SV level software trade studies, common analyses and integration activities tailorable for each mission area and programReview program SV level software engineering work products for consistency Support major technical reviews and failure investigations as an Independent ReviewerMentor and train program SV level Software Engineers Hold monthly working group meetings across program SV level software engineers to share lessons learned, best practices, ongoing concerns/issues, and potential opportunitiesEnsure engineering excellence on executing programs through consistent and repeatable SV level software engineering integration activities across the Sector25% travel as requiredQualifications: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 software performance analysis such as processor and memory utilization, data sizing and flows, etc.Integrated Space Vehicle Software CSCIs for end-to-end mission performanceInternal and external software interface managementSpace vehicle fault management architectures and designLeading both internal and external supplier engineering teamsSoftware/Firmware integration with hardware, testing, and troubleshooting Preferred Additional Skills:Test bed and simulator design processWell versed in fleshing out physical and functional interface details such as data formats and software protocolsFamiliarity with SW engineering processes such as Agile/Waterfall, DevSecOps, Cont Integration as well as SW development related to embedded/RT/architecture patternsWell versed in functions, responsibilities and interconnectivities between SV SW, Ground SW, Test SW and Operations SWFamiliarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRAStrong 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, & demonstrationAbility to make risk-based decisions balancing technical, cost and scheduleFamiliarity with ConOp development Accustomed to leading technical engagement with internal and external customers in formal presentations as well as informal table-top discussionsExcellent communication and presentation skills and the ability to work harmoniously in a team environment with government customers and other contractorsProven analytical and troubleshooting skills demonstrated by related work experienceStrong coordination and organization skills with a focus on detailsStrong track record of leading software engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operationsExperience in mentoring and growing technical staffIn 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 Integration and Test Systems Engineer (Active TS/SCI Clearance Required)Job Code: 10692Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CAJob 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 ICDsDesigns 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 discrepanciesGenerates comprehensive documentation, test reports, and data analysis to communicate the results of integration and testing activitiesIdentifies potential risks and develops mitigation strategies to ensure the successful integration and testing of the space vehicleExtracts 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 programsSupport to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generationWorks 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 lifecycleRepresent 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 MDRLeads failure review boards, engineering review boards, change control boards to ensure mechanical impacts are coordinated across the SVCreating and/or supporting delivery of Customer CDRLS25% travel as requiredAbility to lead diverse technical teams across internal and subcontractor effortsQualifications: 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 pathsExperienced with space vehicle, test bed/simulators, EGSE, and MGSE requirements validation, sell-off, milestone entry/exit criteriaFamiliarity with Digital Engineering and MBSE tools such as CAD, DOORs, CAMEO, CREO, JIRAAbility to make risk-based decisions balancing technical, cost and scheduleAbility to support Space Vehicle level electrical, mechanical, and software analyses and tradesStrong 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 operationsExperience in mentoring and growing technical staffIn 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 Software Systems Engineer (Active TS/SCI Security Clearance Required)Job Code: 10696Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CAJob Description: L3Harris' Space and Airborne Systems seeks a Space Vehicle (SV) Software Systems Engineer (SWSE) to join our growing team. The individual in this position will serve as the lead software systems engineer for integrating numerous software CSCIs across the spacecraft bus, mission payload, and communications payload to ensure seamless end-to-end mission performance when interfacing Ground, Operations and Test SW CSCIs. The SWSE has overall technical responsibility for the software 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 SWSE will coordinate and/or perform test and analysis integration activities to ensure the system meets Customer and Mission requirements. The SWSE will coordinate all software technical efforts to generate contractually required system design documents and design review technical packages. Essential Functions: Manages and maintains integration of SW & FW w/ HW across all aspects of the SV and according to internal and external ICDsGeneration and coordination of software design specifications and interface (internal and external) documents including requirements derivation, allocation, and flow up/down, and V&V activitiesExtracts software 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 integration activities such as processor/memory utilization, data sizing, etc.Supports the SEIT organization in planning the integration testing of HW/SW from the subsystem level to the SV level, including execution of SV level tests and troubleshooting issuesMaintains cognizance and communicates changes of the SV subcontractor and in-house Firmware and Software baselines. Support to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generationWorks closely with Electrical, 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 lifecycleRepresent Space Vehicle software engineering during major system level design reviews such as SRR, SDR, PDR and CDR and milestone reviews such as MRR, TRR, PSF, LRR and MDRLeads or participates in failure review boards, engineering review boards, change control boards to ensure software impacts are coordinated across the SVCreating and/or supporting delivery of Customer CDRLSAbility to lead diverse technical teams across internal and subcontractor efforts25% travel as requiredQualifications: 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 Software Engineering, Systems Engineering, or adjacent field.Active TS/SCI security clearance. Experience with integrated Space Vehicle Software CSCIs for seamless end-to-end mission performance.Experience with leading both internal and external supplier software engineering teams.Experience with Software/Hardware integration, testing, and troubleshooting of complex systems.Preferred Additional Skills: Well versed in fleshing out physical and functional interface details such as software and communication protocols, data rates, data formats, data and bit structures, application programming interfaces (API), and error handling mechanismsExperienced with software requirements validation, sell-off, milestone entry/exit criteriaExperienced with software integration planning when there are multiple SW/HW solutions in the loopExperience with writing Statement of Works for external and internal suppliersFamiliarity with SW engineering processes such as Agile/Waterfall, DevSecOps, Cont Integration as well as SW development related to embedded/RT/architecture patternsFamiliarity with Digital Engineering and MBSE tools such as DOORs, CAMEO, CREO, JIRAStrong track record of leading software engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operationsAbility to make risk-based decisions balancing technical, cost and scheduleAbility to perform Space Vehicle software analyses and trades such as processor and memory utilization, data sizing and flows, fault management techniques, etc.Experience in mentoring and growing technical staffIn 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: 10697Job Location: Remote or Palm Bay, FL or Rochester, NY or Ft. Wayne, IN or Colorado Springs, CO or San Diego, CAJob 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 ICDsGeneration and coordination of electrical design specifications and interface (internal and external) documents including requirements derivation, allocation, and flow up/down, and V&V activitiesExtracts 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 analysesSupports 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 issuesMaintains cognizance and communicates changes of the SV subcontractor and in-house electrical design baselines, pinouts, and interfacesSupport to the system modeling teams in generation of Cameo system views and simulations as well as ConOps generationWorks 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 lifecycleRepresent 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 MDRLeads or participates in failure review boards, engineering review boards, change control boards to ensure electrical impacts are coordinated across the SVCreating and/or supporting delivery of Customer CDRLSAbility to lead diverse technical teams across internal and subcontractor efforts25% travel as requiredQualifications: 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 criteriaExperienced with software integration planning when there are multiple SW/HW solutions in the loop, including flight and test harnessesExperience with writing Statement of Works for external and internal suppliersFamiliarity 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, JIRAStrong track record of leading electrical engineering teams through all phases of a space program; pursuits and proposal, design and development, integration and test, and operationsAbility to make risk-based decisions balancing technical, cost and scheduleAbility 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 analysesExperience in mentoring and growing technical staffIn 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.