2 ms·

Um, the moon also has no atmosphere. We were able to land on that in the 60's. https://en.wikipedia.org/wiki/VTVL https://en.wikipedia.org/wiki/VTVL. Lots of

• sgt101 2y ago
  But the moon is 1/9th the mass of Mars (approx) The moon has an average orbital velocity of 1km per sec (approx) Mars is 24km per sec (approx) Terminal velocity is 600ms, on earth it's 54ms So we are talking about something that is an order of magnitude more difficult. I think if retro rockets are to be used then far more fuel will be needed. But that means far more mass, which means more fuel - how much fuel would be needed to slow something like Starship for example?
  • 00N8 2y ago
    Many of the landers we've already put on Mars are heavier & less tolerant of G forces than a human, so it's clearly not an insurmountable hard limit. They use a combination of parachutes, retro rockets & airbags usually. But you're right that the lander stage has to be a small fraction of the size of the interplanetary stage, & the economics aren't very good. Maybe you'd need to send several Starships to Mars orbit to refuel & support a single one landing &/or returning to Earth -- at least until refueling facilities exist on the surface, & assuming Starship is actually capable of this mission.