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
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...