CLLARE Command Module structure

From CSTART Wiki

Currently essentially nothing is known about the structure of the CM.

If you are a structural engineer or someone with equivalent knowledge/experience and you think you can help us to design a CM structure which is cheap, light and appropriate for:

  • Forces and vibration acting on the CM during launch
  • Pressure difference between pressurised crew cabin and external vacuum
  • Radiation exposure during trans lunar trajectories
  • Low tetmperature extremes in space
  • High temperature extremes during reentry

and other relevant concerns, please introduce yourself on the forums and begin posting in the Spacecraft Engineering Workgroup forum.

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