Lead system-level EMC/EMI analysis for satellite and aerospace systems, including mission requirements, spacecraft cavity geometry, and DC/RF coupling effects
Perform conducted and radiated emissions and susceptibility (CE/CS, RE/RS) analyses to ensure compatibility with satellite and launch vehicle environments
Conduct magnetic field, surface charging, and internal charging analyses
Evaluate spacecraft panel shielding effectiveness and recommend design improvements
Develop, review, and oversee EMC/EMI test plans for system verification and validation
Collaborate with systems engineers, payload designers, and integration teams to ensure EMC/EMI compliance throughout the project lifecycle
Mentor junior engineers and provide technical leadership for EMC/EMI engineering activities
Prepare technical documentation and ensure compliance with applicable aerospace standards
Requirements
Bachelor's degree in Electrical Engineering or Aerospace Engineering (Master's or Ph.D. preferred)
7–10 years of experience in EMC/EMI analysis and testing for satellite or aerospace systems
Strong experience with: System-level EMC/EMI analysis, Conducted and radiated emissions/susceptibility (CE/CS, RE/RS), Magnetic field, surface charging, and internal charging analysis, Spacecraft panel shielding effectiveness, EMC/EMI test plan development and validation
Proficiency with EMC/EMI simulation and analysis tools such as CST and FEKO
Knowledge of satellite mission requirements, including frequency bands, payloads, and antenna systems
Familiarity with aerospace EMC standards, including: MIL-STD-461, MIL-STD-464, ECSS-E-ST-20-07C
Strong analytical, problem-solving, communication, and leadership skills with the ability to work independently and mentor engineering teams
Benefits
On-site preferred; remote or hybrid may be considered for exceptional candidates