CLLARE Command Module aerodynamics

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

If you are an aeronautical engineer or someone with equivalent knowledge/experience and you think you can help us to model:

  • Dyanmic pressure on the CM hull during launch
  • Stable reentry positions for the CM
  • Lift generated by the CM during reentry at various attitudes
  • Drag generated by the CM during reentry at various attitudes

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

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