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.