NASASpaceFlight.com Forum
SLS / Orion / Beyond-LEO HSF - Constellation => Missions To Mars (HSF) => Topic started by: Von Carlo on 06/27/2008 09:09 am
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Hi everybody!
Is someone able to help me in finding expected values for ARES V max g-loads ("quasi-static" and dynamic, axial and lateral) during a Lunar mission?
Thanks so much
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Still apt to change, AFAIK. I believe I read somewhere that the new six-engine configuration would produce 4.3g at MECO. But since that design doesn't meet the performance specification it will need to be changed... again...