M
mikejz
Guest
Given that the the velocity of Direct-Entry to Mars is around 5.4km/s (Modest compared to a return lunar entry). And several proposed variants of the CEV include a airbag system for ground landing; Is it conceivable that with the addition of a significant retro rocket system and changes in the parachute system that a CEV could actually be used for entry and landing on Mars in a flat terrain area?