Thermal Engineer

Spaceodysseyhub; Toulouse; Sur place; EUR 60 000 - 80 000; Plein temps

Résumé du poste

Spaceodysseyhub in Toulouse is seeking an experienced Thermal Engineer to control the temperature of spacecraft components and lead thermal analysis. This role involves both analysis and hardware design, focusing on cryogenic detectors and lithium-ion battery packs.

The ideal candidate will have 5–8 years of relevant experience and proficiency in tools like Thermal Desktop, Python, and MATLAB. Responsibilities include designing thermal control systems and performing tests to ensure component integrity under extreme conditions.

Qualifications

• 5–8 years of experience in spacecraft thermal engineering (analysis and hardware design).
• Proficiency in Thermal Desktop, ESATAN‑TMS, or equivalent thermal network solvers.
• Experience with Python scripting, MATLAB, NumPy, Pandas, and Matplotlib for telemetry analysis.

Responsabilités

• Control the temperature of spacecraft components, including cryogenic detector arrays and lithium‑ion battery packs.
• Perform thermal analysis using tools such as Thermal Desktop, ESATAN‑TMS, and Python/MATLAB for telemetry post‑processing.
• Design and size radiator panels, multi‑layer insulation (MLI) blankets, and heater circuits.

Description du poste

Keep cryogenic detectors cold and electronics bays alive through 150°C orbital swings.

Spacecraft thermal engineers control the temperature of every component aboard a mission — from cryogenic detector arrays that must stay at 4K to lithium‑ion battery packs that must never exceed 25°C during peak recharge. The discipline is 70% analysis (thermal desktop orbital heating models, SINDA/FLUINT transient network solvers, Monte Carlo Radiative Analysis) and 30% hardware (multi‑layer insulation (MLI) blanket design and installation, radiator panel sizing, thermal interface material (TIM) selection, heater circuit design with thermistors and thermocouples). Familiarity with Python scripting and MATLAB for post‑processing thermal telemetry is now standard.

Career Journey

5 milestones in the career path.

1. Bachelor’s in Mechanical Engineering, Aerospace Engineering, or Physics (~4 years). Heat transfer (conduction, convection, radiation), thermodynamics, and fluid mechanics form the essential foundation. Undergraduate research in thermal measurements or CFD is highly valued.
2. Master’s in Thermo/Spacecraft Thermal Engineering (~2 years). Learn Thermal Desktop or ESATAN‑TMS. Thesis involving orbital thermal modelling or cryogenic system design gives a strong entry profile.
3. Junior Thermal Engineer – component and board‑level thermal modelling (~2 years). Build thermal models for electronics boxes, run worst‑case hot/cold analysis for PDR, size heater circuits and select thermistors, and participate in TVAC chamber testing campaigns.
4. Senior Thermal Engineer – subsystem and vehicle thermal control system (~3 years). Own the spacecraft thermal control system (TCS) from Phase B through launch, size radiators, design MLI blanket layout, write the thermal analysis report, and lead the TVAC acceptance and qualification test campaigns.
5. Principal / Lead Thermal Engineer (~2 years). Define thermal architecture for new platforms or missions, review and approve subsystem thermal models, develop thermal margins policy, and support on‑orbit anomaly resolution via telemetry analysis and model updates.

Key Responsibilities

• Control the temperature of spacecraft components, including cryogenic detector arrays and lithium‑ion battery packs.
• Perform thermal analysis using tools such as Thermal Desktop, ESATAN‑TMS, SINDA/FLUINT, and Python/MATLAB for telemetry post‑processing.
• Design and size radiator panels, multi‑layer insulation (MLI) blankets, and heater circuits with appropriate thermal interface materials.
• Lead thermal‑vacuum (TVAC) acceptance and qualification test campaigns.
• Analyze on‑orbit thermal anomalies, reconstruct changes, and update models using limited telemetry data.

Required Skills & Experience

• 5–8 years of experience in spacecraft thermal engineering (analysis and hardware design).
• Proficiency in Thermal Desktop, ESATAN‑TMS, or equivalent thermal network solvers.
• Experience with Python scripting, MATLAB, NumPy, Pandas, and Matplotlib for telemetry analysis.
• Knowledge of ESA ECSS‑E‑ST‑31C for MLI blanket emissivity and installation specifications.
• Familiarity with SINDA/FLUINT for coupled thermal–fluid systems (heat pipes, cryogenic loops).

Ideal Candidate

Good fit if you are drawn to physics‑based simulation, enjoy multidisciplinary work spanning radiation physics, materials science, cryogenics, and electronics packaging, and are patient and methodical. Bad fit if you dislike analysis‑heavy work, desire rapid product feedback, or prefer steady‑state environments.

Challenges

The hardest part is on‑orbit thermal anomaly resolution with insufficient telemetry. Engineers must reconstruct changes with limited data and no hardware access, requiring deep understanding of thermal interfaces, shadow effects, and sensor calibration.