On Wed, 2 Oct 2013, Aplin Alexander T wrote: > Musk pointed out during the post-flight Q&A that "I believe the first > time that any rocket stage has attempted to do a supersonic > retro-propulsion." Apparently it was successful (this was the 1st > stage's initial 3-engine re-entry burn). If you interpret "retro-propulsion" in the specific sense of firing main engines forward while still in detectable atmosphere, yeah, I think that's true. Kistler was going to do it, but they never flew. Nor did the shuttle ever do an RTLS abort. The Apollo LM did supersonic retro-propulsion down to landing, but that was in vacuum. And many rocket stages have fired small solid-fuel retros as part of stage separation, but that's not quite the same thing either. > IIRC super-sonic retro-propulsion is one of the unknowns encountered in > planning manned (and other large-payload) landings on Mars. Yes, there's a problem with the Martian atmosphere just not being thick enough to brake a big lander (with a lot of mass behind every square meter of forward surface) adequately. Supersonic retro-propulsion seems to be the current favorite answer to this. (One caveat: I've never seen a detailed analysis of the problem with the assumptions explicitly stated and justified. I have a faint suspicion that possibly-feasible alternatives may have been neglected because supersonic retro-propulsion was the pre-chosen winner.) > I've always been surprised than no one's tried it before - is it > something amateur rocketry could investigate here on earth? If you mean doing tests that would actually be relevant to stage return and/or Mars descent, I think it would be a considerable challenge, because you have to start high up, in thin air, moving fast. Just getting to those initial conditions isn't easy for amateurs. Henry Spencer henry@xxxxxxxxxxxxxxx (hspencer@xxxxxxxxxxxxx) (regexpguy@xxxxxxxxx)