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I have in
front of me right now, a drawing that Owen left me, of the "Radial "Module All-Rigid Space Station" that one of the draftsment did for him in 1962; designed to be launched on a Saturn V, using a ciyple of "6-man ferry-logistics vehicles" docked to it, basically an Apollo CSM. Owen also prepared (and patented) a design for a trans-Mars space station based on this design (I think that one was planning on using a NERVA upper stage to push it out to Mars and back again)---this was actually released by one of the commercial model companies as a plastic kid's model in the 1960s, as "NASA's Space Station." MPC's Pilgrim Observer. One of the best fictional spacecraft kits ever made. Gene |
#12
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![]() wrote in message oups.com... MPC's Pilgrim Observer. One of the best fictional spacecraft kits ever made. A quick Google search brings up a page with pictures. Very cool looking design. http://www.greysteele.com/models/pilgrim.htm Jeff -- Remove icky phrase from email address to get a valid address. |
#13
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In article ,
John Savard wrote: The original specs for what became the CSM called for missions in Earth orbit and lunar orbit... but not a landing. And, of course, that means that if the Saturn V could be pressed into sending men to the Moon, the later rocket, had it been developed, would have been, if not well suited to, at least capable of, sending men to Mars. Careful here. The Saturn V appeared *after* the goal changed to a landing. Those original CSM specs envisioned flying on a Saturn I, and later on one of various concepts for a Saturn II. Circumlunar flights were thought to require orbital assembly, and any lunar landing would probably require both orbital assembly and a larger launcher, plus perhaps a small space station as an assembly base. Only after the goal became more ambitious and the schedule was greatly compressed did the rockets start to balloon in size. The Saturn V was *enormous* by the standards of the early planning -- bigger than most of the old Nova concepts for Saturn follow-ons -- and shared only the name and a few odds and ends of hardware with the original Saturn concepts. And at that, using two *Saturn Vs* with orbital assembly was the baseline concept for a while. As it is, though, we have Dr. Zubrin who came up with a way to make even the mere Saturn V capable of sending men to Mars. The Saturn V was perfectly capable of sending men to Mars, provided you didn't insist on doing it with a single launch. Orbital assembly simply would come back into the picture at that point. (Note that even Zubrin's ideas need two launches -- he just does the assembly on Mars instead of in Earth orbit. Not everyone agrees that this is the best approach.) -- "Think outside the box -- the box isn't our friend." | Henry Spencer -- George Herbert | |
#14
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In article ,
Derek Lyons wrote: There is nothing modular about the Apollo spacecraft. The CSM is a matched pair always and forever. Wasn't there some non-trivial thoughts about a light-weight mini-SM for use with Earth-orbit missions like Skylab? There was. But substituting a SM late in the game isn't the same as designing a modular system. And likewise, designing a modular system which ends up only existing in one version isn't the same as designing a non-modular system. Note that Owen Maynard, who Kieran was quoting, was there, and you weren't. Hint: think of what the M stands for in CM, SM, LM. -- "Think outside the box -- the box isn't our friend." | Henry Spencer -- George Herbert | |
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#16
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On Thu, 09 Dec 2004 23:08:37 GMT, "Greg D. Moore \(Strider\)"
wrote: .. Hint: think of what the M stands for in CM, SM, LM. And RM. Apollo also used one more Module. Can anyone name it? - Rusty |
#17
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![]() Jeff Findley wrote: A quick Google search brings up a page with pictures. Very cool looking design. http://www.greysteele.com/models/pilgrim.htm The Apollo in the kit has two odd features- its CM is corrugated on the exterior like a Mercury or Gemini, and there's a odd depression on the CM that has a chrome rod set in it. You can see the modified Apollo on this PDF of the instruction sheet; it's on page 4, step 11: http://www.ninfinger.org/~sven/model...ns/mpc9001.pdf The Pilgrim Observer's design has a major problem; there is almost no propellant on board for the three base-mounted J-2 engines. Pat |
#18
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#19
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#20
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![]() "Derek Lyons" wrote in message ... When you do, you note the modularity is defined as 'being able to leave bits not needed behind', something the Apollo spacecraft is decidedly not able to do. Whether it's the super-heavy J mission SM, or the ultra lightweight CRV SM, the CM is wedded always and forever to a SM. Reentry. |
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