Overview

The Thermal Subsystem ensures that all satellite components remain within their designated operating and non-operating temperature limits. To determine these temperature ranges and verify material tolerances, we perform detailed thermal analyses using specialized software. Additionally, we conduct physical tests by subjecting the satellite to a range of controlled thermal stresses to simulate on-orbit conditions.

Position Description

  • Research on the appropriate active and passive thermal control methods for various crucial components
  • Construct a mathematical model of the satellite for thermal analyses
  • Conduct and evaluate a range of essential thermal tests to optimize the current design
  • Utilize thermal analysis software such as ESATAN-TMS and Simcenter to evaluate the satellite’s thermal performance in orbit

Preferred Skills

  • Heat Transfer Theory and Materials Science
  • Control Theory
  • Finite Elements Method (or any other Discretization method for numerically solving differential equations)
  • Experience in systems’ simulation and modeling
  • Experience with laboratory equipment (e.g. PSU, multimeter)
  • A strong sense of commitment and responsibility

Have Questions?

Feel free to reach out if you want to learn more about this position or the project in general.

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