This is a hands-on technical leadership role. You will work closely with the Director of Electrical Engineering, technical leads, Systems Engineering, and Program Management to deliver robust, flight-ready electrical systems.
Responsibilities
Own the technical baseline and architectural direction for electrical and avionics systems across Hardware, Firmware, Harnessing, Launch Vehicle Systems, and Spacecraft Systems.
Define and own spacecraft and launch vehicle electrical architectures, including power generation/distribution/storage, command and data handling, communication interfaces, and harnessing.
Establish, maintain, and enforce electrical engineering design standards, processes, and best practices.
Lead the development, allocation, and management of system and subsystem electrical requirements, ensuring traceability, verification, and validation.
Lead and chair major design reviews (SRR, PDR, CDR, TRR, FRR) and technical risk assessments; sign off on design maturity and readiness.
Drive the common modular architecture effort to maximize reuse and commonality across launch vehicles and spacecraft.
Provide technical direction and oversight to electrical, power, avionics, FPGA/ASIC, firmware, and harness teams; review and approve key design artifacts, analyses, schematics, ICDs, power budgets, and test plans.
Lead trade studies (power architectures, redundancy, component selection, radiation tolerance, derating, thermal/electrical interfaces) to optimize performance, cost, schedule, and risk.
Ensure compliance with space environmental requirements (radiation, EMI/EMC, thermal, vacuum, launch loads) and guide EEE parts selection, qualification, and derating.
Define and guide integration and test strategies, including functional testing, hardware-in-the-loop, environmental qualification (vibration, shock, TVAC, EMI), and system-level verification.
Support failure analysis, anomaly resolution, and root-cause/corrective action during development, integration, test, and on-orbit operations.
Collaborate closely with Systems Engineering, Mechanical, Software, RF, GNC, Mission Assurance, and other disciplines to ensure balanced, integrated vehicle designs.
Support department management with product/technology roadmaps, IRAD direction, proposal technical volumes, BOEs, risk assessments, and new business capture.
Mentor and develop engineers at all levels, promoting rigorous engineering practices and a culture of technical excellence.
Continuously improve internal processes, tools, analysis methods, and design-for-manufacturing/test practices.
Qualifications
Required
Bachelor’s degree in Electrical Engineering, Computer Engineering, Aerospace Engineering, or a closely related field.
15+ years of progressive experience in electrical or avionics engineering for complex aerospace systems (launch vehicles and/or spacecraft), including significant technical leadership responsibility.
Demonstrated experience as technical authority or chief/lead engineer on flight hardware programs, owning architecture and design integrity through development, integration, test, and flight.
Strong technical depth in spacecraft/launch vehicle power systems, avionics/data handling (including common buses such as SpaceWire, CAN, MIL-STD-1553, Ethernet), harnessing, and related disciplines.
Proven experience with EEE parts selection and derating, radiation effects (TID, SEE) and mitigation, requirements management, and space environmental qualification.
Track record leading multi-disciplinary teams, conducting trade studies, resolving complex technical issues, and balancing technical performance with cost and schedule constraints.
Experience taking designs from concept through high TRL / flight qualification, including PCB assemblies, firmware, and system-level integration and test.
Excellent written and verbal communication skills, with the ability to prepare and present complex technical material to engineering teams, leadership, and external customers.
Ability to work effectively in a fast-paced environment and collaborate across multiple engineering disciplines.
Desired
Master’s Degree or Ph.D. preferred.
Direct experience with modular avionics architectures and design-for-reuse across multiple vehicle platforms.
Hands-on background in board-level design, FPGA/ASIC development, or harness design and analysis.
Experience supporting on-orbit operations, anomaly resolution, and post-flight analysis.
Familiarity with configuration management, requirements management tools, and technical baseline control in a flight hardware environment.
Prior experience providing technical content for proposals and supporting new business capture.
Knowledge of relevant industry standards (MIL-STD, ECSS, NASA, or equivalent) and best practices for space electrical systems.
Ability and willingness to obtain a security clearance if required.
Firefly offers outstanding benefits for our employees, including generous health, dental and vision plans with low plan deductibles, parental leave, relocation benefits, educational reimbursement, short term disability, and flexible PTO options.
To conform to U.S. Government space technology export regulations, including the International Traffic in Arms Regulations (ITAR) you must be a U.S. citizen, lawful permanent resident of the U.S., protected individual as defined by 8 U.S.C. 1324b(a)(3), or eligible to obtain the required authorizations from the U.S. Department of State.
Firefly Aerospace, Inc. is an Equal Opportunity Employer; employment with Firefly is governed based on merit, competence and qualifications and will not be influenced in any manner by race, color, religion, gender, national origin/ethnicity, veteran status, disability status, age, sexual orientation, gender identity, marital status, mental or physical disability or any other legally protected status.
