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This role is responsible for thermal system design and analysis of complex spacecraft and payloads, spanning from the lowest‑level component up through sub‑system and full system levels. The position includes designing thermal solutions for a wide range of electronic components and ensuring thermal closure while meeting cost and schedule objectives.
Job Responsibility
Perform thermal system design and analysis for spacecraft and payloads across component, sub‑system, and system levels
Design thermal integration of electronic components such as processors, power supplies, cameras, and optical assemblies at the sub‑system and spacecraft level
Ensure thermal designs close properly and identify innovative technical means to meet thermal, cost, and schedule requirements
Perform FEM‑based thermal model analysis using Thermal Desktop
Develop preliminary concepts supporting early design activities through design V&V (verification & validation) and transition to rate production
Collaborate effectively with avionics, mechanical, structural, program management, and AI&T teams
Requirements
Bachelor’s degree or higher in a relevant engineering or computation field plus 8–10 years
MS plus 6–8 years
PhD plus 3–5 years of professional experience in thermal engineering positions
3+ years of professional working experience in the space industry
Experience with Thermal Desktop
CAD modeling
basic thermal principles
Nice to have
Ability to perform mechanical engineering design tasks using SolidWorks