Bachelor’s degree in aerospace, mechanical, electrical engineering or any equivalent combination of education and experience
8+ years of experience in the architectural design, development, test, and integration of space-grade avionics systems
Experience programmatically interfacing with hardware test automation and data analysis tasks
Ability to work in a fast-paced and high velocity start-up atmosphere
Creative problem solver that can assess risk and make collaborative design and development decisions
Hands-on experience with environmental testing for space electronics and harnessing such as thermal, thermal vacuum, vibration, shock, radiation, and EMI/EMC testing per SMC-S-016
Expertise with vehicle grounding architecture, spacecraft charging, EMI, and/or RF testing and compatibility
Competence with electrical test equipment (multimeters, oscilloscopes, network analyzers, etc.)
Strong presentation experience in highly technical design forums and reviews (Preliminary Design Reviews, Critical Design Reviews, Flight Readiness Reviews, etc.)
Proficient with NX or similar CAD software including electrical harness routing
Expertise in PCB schematic capture and board layout, ideally using Altium or similar software
Experience with Linux, Bash, C++, MODBUS
Experience with vehicle level testing including writing test procedures, creating robust and efficient test sequencing, and analytical data review to evaluate hardware health
Familiarity with vehicle power analysis, flight software state machine structures, and communication systems