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Orion G-force question

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Alan Erskine - 13 Jun 2008 14:53 GMT
What are the launch and re-entry G-forces for Orion?  Surely, a capsule will
be worse than the shuttle.  If they have to use a recumbant seat for ISS
crews returning on the shuttle, will that be sufficient for Orion?  What
about longer-term crews; how will they fair returning on Orion?
charliexmurphy@yahoo.com - 13 Jun 2008 15:26 GMT
> What are the launch and re-entry G-forces for Orion?  Surely, a capsule will
> be worse than the shuttle.  If they have to use a recumbant seat for ISS
> crews returning on the shuttle, will that be sufficient for Orion?  What
> about longer-term crews; how will they fair returning on Orion?

No issue here

The Orion "couches" are recumbent by definition

No different than the Soyuz that have been used for long term station
residents before the shuttle existed and since
Brian Gaff - 14 Jun 2008 08:33 GMT
Well cannot be worse than Soyuz of late and nobody has died from the g
forces yet!

Brian

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> What are the launch and re-entry G-forces for Orion?  Surely, a capsule
> will be worse than the shuttle.  If they have to use a recumbant seat for
> ISS crews returning on the shuttle, will that be sufficient for Orion?
> What about longer-term crews; how will they fair returning on Orion?
balpao@gmail.com - 16 Jun 2008 23:26 GMT
> Well cannot be worse than Soyuz of late and nobody has died from the g
> forces yet!
[quoted text clipped - 10 lines]
> > ISS crews returning on the shuttle, will that be sufficient for Orion?
> > What about longer-term crews; how will they fair returning on Orion?

I think that more than g-force is important that is possible to abort
the launch at any time.  The soyuz design forgive an incredible range
of possible problems. Simple and stupid, but very robust.

They can go out of route of undred of kilometers and still survive.

Or they can survive an incredible mess like this:

http://www.astronautix.com/flights/soyuz181.htm

If it was the shuttle they could have die a dozen of times.

The soviets didn't divulgate what they considered an unsuccesful
launch. But as for me this is the the most succesful example of how a
good design for manned space flight has to be.  Simple, robust and
having a low energy abort mode at almost any time of the flight, even
if you do many mistakes.
Brian Thorn - 16 Jun 2008 23:33 GMT
>I think that more than g-force is important that is possible to abort
>the launch at any time.  The soyuz design forgive an incredible range
>of possible problems. Simple and stupid, but very robust.

And yet it has suffered the same number of fatal accidents as the
Space Shuttle.

Brian
balpao@gmail.com - 17 Jun 2008 00:48 GMT
On 17 Giu, 00:33, Brian Thorn <bthor...@suddenlink.net> wrote:
> >I think that more than g-force is important that is possible to abort
> >the launch at any time.  The soyuz design forgive an incredible range
[quoted text clipped - 4 lines]
>
> Brian

Sorry, my english is bad.

I've not data... I know about soyuz 11 accident in 1971 but recently
(say,the last 30 years) I don't remember fatal Soyuz missions.

A complicated thing like STS contains so many points of failure that
it requires an incredible good work to operate it. It contains many
parts, and the failure of just one of them could be fatal. So failure
rate of any single piece and tollerances have to be extremely good.
Probability is on the side of "simple" veichles.

I expect that Orion will be more Soyuz (but also Apollo) like in the
sense that it will be much more simple and robust.

And it will forgive a lot of mistakes. Russians made incredible
mistakes during some missions, but despite this they very often saved
the crew.

A capsule is intrinsecaly more safe.  I linked Soyuz 18-1 as an
extreme example, but also Apollo 13 is a story of fantastic
robustness.

A manned launch has to do just one thing: take humans to space and
back in the more simple and safe way. Never mind it's not "sexy".

Cargo and other stuff could be launched in separated launch, as they
are more expendable.

The topic is about g-forces.  When Soyuz does a ballistic reentry it
can reach 10 g.  I simply expect that Orion could  withstand even more
weird reentries than this. Human body can resist a lot of g.
Hopefully it will never be required, but in case better sick than
disintegrated.

This time is better to do it more robust with less frills.
 
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