pete...@gmail.com wrote in
news:81cbce99-8afc-40da...@googlegroups.com:
> On Thursday, April 30, 2015 at 1:39:05 PM UTC-4, Gutless
> Umbrella Carrying Sissy wrote:
>> Cryptoengineer <
treif...@gmail.com> wrote in
>>
news:XnsA48BD39536...@216.166.97.131:
>>
>> > I have to say I'm find this a little confusing. We have
>> > actual rocket scientists telling us can't land on Mars on
>> > retros, yet Elon Musk's Falcon boosters are getting close to
>> > sucessful landings, purely on retros. No parachutes involved.
>>
>> And showing that it is a very difficult task, even when the
>> flight time is minutes, at earth normal temperatures, without
>> having to deal with the effects of months in a vacuum.
>> Impossible, so far, in fact.
>
> It looks like an iterative debugging process, and I don't think
> there's much doubt they'll figure it out. The next test is in
> June.
I agree. But it shows that doing the same thing at a range of 35
million miles (or more) is *hard*.
>
>> > Perhaps
>> > they are moving at a lower velocity, though Musk is also
>> > talking about recovering the second stages, which do reach
>> > orbital velocity.
>>
>> I'm not sure what the final speed is on the first stage, but
>> yeah, it's a *lot* slower than orbital. And remember, the
>> reasons for the failures so far are, for the most part,
>> expendable supplies. Specifically, fuel and hydraulic fluid.
>> Add enough of both to land properly from orbital speeds, and
>> you likely won't be able to launch at all due to the weight.
>
> SpaceX also plans to retrieve the second stage, which does reach
> orbit. They haven't started on that one yet.
And there are a number of "companies" that plan to mine the moon
for, I'm not sure what, or mine asteroids for platinum, or
whatever. Planning to do so and doing so are not necessarily even
remotely connected.
(That said, if anybody can pull it off, it's SpaceX, but you're
talking a job that's a *lot* more challenging - the first stage
isn't making any kind of reentry.)
>
>> And this is all with the action happening close enough for
>> realistic real time control, rather than a half hour delay.
>> >
>> > Part of the Mars problem is that ships have been going into
>> > EDL as soon as they arrive, with the full velocity of their
>> > interplanetary trip. One of the mitigations the engineers
>> > are proposing involves a preliminary aerobrake pass through
>> > the upper atmosphere and settling into low Mars orbit
>> > before final EDL.
>> >
>> Interesting thought, if the numbers work out. But don't lower
>> orbits require _higher_ velocities? So reentry from the lower
>> orbit would actually exaggerate the problem of slowing down,
>> because the initial speed would be higher.
>
> The real rocket scientists seem to think this is the right way
> to do it. If you start in high orbit, you've farther to fall to
> get to the atmosphere, and I suspect the speed gained in that
> fall is the same or higher as the speed of the lower orbit -
> after all, you've more potential energy to get rid of.
I think the main advantage is that you don't have to take the mass
of what you're slowing down against (air) with you. That's a big
advantage. But if it were obviously the best course, they'd have
been doing it all along.
>
> Deorbiting starts with a retro rocket burn to kill your orbital
> velocity.
No. Deorbiting starts with a retro rocket burn to slow your orbital
velocity to below orbital velocity. On the moon, yeah, you need to
kill it completely. On Mars, even with its thin atmosphere, not so
much.
Which is to say, it's complicated and difficult, under the best of
conditions, which is why we have a 50% failure rate on Mars
landers.