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There has been some talk of a substitute for Orion/Constellation that
would include a manned spacecraft that would be used solely in space (i.e. no descent/reentry module). I assume it would fly between earth orbit and moon orbit or mars orbit. Can anyone point me to a details, design, etc.? |
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On Apr 13, 9:50*am, wrote:
There has been some talk of a substitute for Orion/Constellation that would include a manned spacecraft that would be used solely in space (i.e. no descent/reentry module). *I assume it would fly between earth orbit and moon orbit or mars orbit. *Can anyone point me to a details, design, etc.? I would imagine that such a vehicle has been sketched, but details may not have been supplied yet, even by the sketcher. Moon-to-LEO returns are problematic due to the braking required; Apollo needed the upper atmosphere drag, and I recall that sci.space.* has discussed the worry on Apollo 13 that they might not be able to get a course that slowed the capsule enough. So inter-orbit may be LEO-MEO or even LEO-LEO. You might want to look up previous information on the space tug ideas. /dps |
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On Apr 17, 2:32�pm, snidely wrote:
On Apr 13, 9:50�am, wrote: There has been some talk of a substitute for Orion/Constellation that would include a manned spacecraft that would be used solely in space (i.e. no descent/reentry module). �I assume it would fly between earth orbit and moon orbit or mars orbit. �Can anyone point me to a details, design, etc.? I would imagine that such a vehicle has been sketched, but details may not have been supplied yet, even by the sketcher. Moon-to-LEO returns are problematic due to the braking required; Apollo needed the upper atmosphere drag, and I recall that sci.space.* has discussed the worry on Apollo 13 that they might not be able to get a course that slowed the capsule enough. �So inter-orbit may be LEO-MEO or even LEO-LEO. You might want to look up previous information on the space tug ideas. /dps picture a inflatable transhab inflated just for braking............ |
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