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Old March 8th 07, 03:18 PM posted to sci.space.history,sci.space.policy,sci.space.station,sci.space.shuttle
Danny Deger
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Posts: 530
Default The 100/10/1 Rule.


"Danny Deger" wrote in message
...

"Reunite Gondwanaland (Mary Shafer)" wrote in
message ...
On Sun, 04 Mar 2007 20:46:23 -0600, kT wrote:

However, one can argue that the expendable SSTO approach puts almost an
order of magnitude more mass into orbit, which is what I am suggesting.


Has anyone ever put anything into orbit with a single stage? I know
we've managed SSTS, Single Stage To Space, but I don't think we've
managed SSTO.


I don't think so. SSTO requires engines for efficent than we have and
requires fuel tanks lighter than we have. Both of these technologies need
to be developed to make a SSTO space craft. NASA tried to develop these
technologies a few year ago and failed in both. I don't know if there is
even a concept out there to make SSTO possible.


I stand corrected on this. An expendable SSTO is very feasible. The X-33
had problems in large part because it also was attempting to do an
atmospheric entry. The entry requirement added a lot of mass to the system.

Danny Deger