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Commentary: Space: At NASA, a return to Apollo?
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Commentary: Space: At NASA, a return to Apollo?
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Soyuz Evolution (was Commentary: Space: At NASA, a return to Apollo?)
On Fri, 12 Sep 2003 16:43:18 +0000, Derek Lyons wrote:
Well, this is utterly untrue. The current Mark of Soyuz is very different from it's ASTP ancestor and wildly different from the original. Here's a little research on that based on Mark Wade's site: The original Soyuz 7K-OK was modified somewhat after Komarov's death in Soyuz 1 but was used for 13 flights. The 7K-OKS was used for the first two Salyut missions. It was basically a 7K-OK with the addition of a lightweight docking system and a crew trasfer tunnel. After the Soyuz 11 accident (depressuration on re-entry) the next design was the Soyuz 7K-T. The major changes were a reduction of crew size from 3 to 2 to allow pressure suits to be worn during re-entry, and a change from solar cells to battery power. Soyuz flew 31 times between June 1972 and May 1981. The ASTP Soyuz 7K-M was a slightly modified 7K-T with the changes needed for ASTP (docking adapter, optical aids, antennae) and solar panels instead of batteries. The next version was the Soyuz T, the crew size went back to the original 3. Comparing the Soyuz T to the 7KT-OK: Improvements were made to the design life (from 10 days to 14 days) and the orbital storage life from 35 to 180 days). The dimensions were the basically the same (the T was slightly shorter in length). The total mass went up from 6,790 to 6,850 kg. Propellant load went from 500 to 700 kg. The primary engine thrust decreased from 417 to 400 kgf. Main Engine Propellants were changed from Nitric Acid/Hydrazine to N2O4/UDMH. Main Engine specific impulse went up from 282 to 305 sec, and total spacecraft delta v from 210 m/s to 320 m/s. The electrical system power increased about 20% primarily because the solar panels were somewhat larger. Most of the improvements were upgrades in electronics, control was now digital, and the telemetry rate was improved. On the other hand the basic configuration was actually closer to the original 7K-OK(S) than the "interim" 7K-T. The Soyuz T first flew in December 79, and the last was in March-July 1986. The Soyuz TM had some improvements over the TM. Updated docking systems for example. There were some materials improvements, the metal sections were stronger, and the heatshield material was lighter. The overall spacecraft was slightly heavier however. The overall dimensions and interior volumes were unchanged. The TM was used on all Mir missions starting in February 87 and for ISS missions until Soyuz TM-34 from April to November 2002. The latest Soyuz TMA is a modified TM to meet NASA requirements for more latitude for Crew height and weight, and an improved parachute system. To date it's been launched twice, and landing once returning the ISS Expedition 6 crew. TMA-2 is still docked with ISS having brought the current Expedition 7 crew of Malachenko and Lu. So just how different is the current Soyuz from the original? The basic dimensions and configuration are pretty much identical, there have been improvements in electronics, engines, and materials. Actually the "interim" Soyuz 7K-T was the farthest from the original since it was the only Soyuz with a two-man crew and without solar cells. I think that an interesting comparison could be made between the Soyuz and the B-52. Today's Soyuz is no more different from it's ancestor than the B-52H flying today is from the original B-52, and probably less so. Of course the B-52 is 15 years older. Even sticking to "capsule" spacecraft, there's a much bigger difference between Mercury, Gemini, and Apollo than between the Soyuz variants. I'm reminded of an interesting comment which David Weeks made to me this summer. He'd been doing a lot of research on the Apollo CSM for the Space In Miniature book which was released this year. He said that he was struck by how much Apollo was the logical design successor to Mercury and that Gemini had been a side-path. Despite the similarity in "look" between Mercury and Gemini, There were more configuration similarities between the Mercury and the Apollo CM than between Mercury and Gemini. |
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Soyuz Evolution (was Commentary: Space: At NASA, a return to Apollo?)
In article ,
Rick DeNatale wrote: ...He said that he was struck by how much Apollo was the logical design successor to Mercury and that Gemini had been a side-path. Despite the similarity in "look" between Mercury and Gemini, There were more configuration similarities between the Mercury and the Apollo CM than between Mercury and Gemini. This is not actually too surprising. Apollo's basic design was fixed at a time when Mercury was only just starting to fly, and it was designed and built by a different company, while Gemini (originally Mercury Mark 2) was based firmly on actual Mercury flight experience and was put together by the same folks who did Mercury. So Apollo really had little opportunity to learn from Mercury's mistakes, and hence repeated a number of them, while Gemini was explicitly meant as "Mercury done right". Mercury and Apollo were both first-generation designs, while Gemini was definitely second generation. -- MOST launched 1015 EDT 30 June, separated 1046, | Henry Spencer first ground-station pass 1651, all nominal! | |
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Commentary: Space: At NASA, a return to Apollo?
David Lesher wrote:
(Derek Lyons) claims: David Lesher wrote: Don't bet on it. The Soyuz, ancient though it may be, remains in service to this day. Well, this is utterly untrue. The current Mark of Soyuz is very different from it's ASTP ancestor and wildly different from the original. Whoa.... I did not say that. I quoted a wire feed. Please don't attribute it to me.. You forward such a ridiculous article, you take the heat for the contents. D. -- The STS-107 Columbia Loss FAQ can be found at the following URLs: Text-Only Version: http://www.io.com/~o_m/columbia_loss_faq.html Enhanced HTML Version: http://www.io.com/~o_m/columbia_loss_faq_x.html Corrections, comments, and additions should be e-mailed to , as well as posted to sci.space.history and sci.space.shuttle for discussion. |
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Soyuz Evolution (was Commentary: Space: At NASA, a return to Apollo?)
Doug... wrote:
Max went straight from designing Mercury into designing Apollo, and by 1961, with the help of his draftsman-cum-engineer Caldwell Johnson (among others), had generated a set of Apollo drawings that were nearly indistinguishable to the layman from the spacecraft that actually flew to the Moon. No real time allowed there for lessons learned from Gemini to creep into the basic design. Collins refers to this in his book IIRC. And was not Gunter Wendt rehired because the Apollo 1 investigation showed a lack of experience on the part of North American? -- The STS-107 Columbia Loss FAQ can be found at the following URLs: Text-Only Version: http://www.io.com/~o_m/columbia_loss_faq.html Enhanced HTML Version: http://www.io.com/~o_m/columbia_loss_faq_x.html Corrections, comments, and additions should be e-mailed to , as well as posted to sci.space.history and sci.space.shuttle for discussion. |
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Soyuz Evolution (was Commentary: Space: At NASA, a return to Apollo?)
In article ,
says... Doug... wrote: Max went straight from designing Mercury into designing Apollo, and by 1961, with the help of his draftsman-cum-engineer Caldwell Johnson (among others), had generated a set of Apollo drawings that were nearly indistinguishable to the layman from the spacecraft that actually flew to the Moon. No real time allowed there for lessons learned from Gemini to creep into the basic design. Collins refers to this in his book IIRC. And was not Gunter Wendt rehired because the Apollo 1 investigation showed a lack of experience on the part of North American? Wendt was *hired* by NAA, not rehired. He had worked for McDonnell- Douglas during Mercury and Gemini. It was a good move, as far as I'm concerned. -- Do not meddle in the affairs of dragons, for | Doug Van Dorn thou art crunchy and taste good with ketchup | |
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