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#81
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![]() Invid Fan wrote: As I'll be in Russia for a little over a week starting Saturday (6 days in St. Petersburg, 3 or so in Moscow), are there any other interesting space sites to see in the area? I now have Gorky Park on my list ![]() The guy to talk to would be James Oberg- he's been there more than once, and probably could give you a good list of interesting things to see: http://www.jamesoberg.com/ The Monino State Aviation Museum has the Soviet "Spiral" space fighter testbed at it, and pretty much all the other production and test aircraft that Russia built in around the past 50 years. http://www.flymig.com/Monino/ Pat |
#82
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![]() Cardman wrote: Buran doesn't have engines at the back that need protecting. I found some interesting Buran photos that you may desire to closely look at... http://www.lindenhillimports.com/buran.htm That I believe is their only surviving v2 model. Certainly there are major changes design changes from their only Buran v1 model that went into space and back. Here's more stuff on the jet-powered prototype: http://www.buran.ru/htm/bstend.htm http://www.buran.ru/htm/anabst.htm http://www.buran.ru/htm/vrdu.htm Pat Cardman. |
#83
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![]() dmitrik wrote: Incorrect. That is Buran "aerodynamic prototype" test article BTS-02 GLI. It was equippedd with four jet engines to test subsonic flight, approach and landing. http://www.buran.ru/htm/anabst.htm http://www.buran.ru/htm/anabst2.htm The original Buran design was going to have the two top motors to aid it in landing after reentry. The two podded side motors were added to allow it to take off from a runway for tests, and would not have been carried on the shuttle in operational service. The two top motors were deleted from the Buran itself to cut weight, but there was an intention to possibly reintroduce them as an improvement after it entered operational service. I spent a couple of days going through the Russian-language version of the Buran website, and bookmarking all the pages that had interesting drawings, photos, or videos on them- so if anyone is looking for anything interesting about Buran's design, or info on the other Soviet spaceplane (Bor, MiG-105 and Spiral) designs, as well as the Energia booster, I'll see if I have any info on the area of interest in my bookmarks. Pat |
#84
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On Mon, 22 Aug 2005 00:59:13 -0500, Pat Flannery
wrote: Here's more stuff on the jet-powered prototype: http://www.buran.ru/htm/bstend.htm http://www.buran.ru/htm/anabst.htm http://www.buran.ru/htm/vrdu.htm There is lots of good information on that site I see. This includes some launch and landing video. Not to mention some better Buran landing photos. Cardman. |
#85
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![]() Cardman wrote: There is lots of good information on that site I see. This includes some launch and landing video. Not to mention some better Buran landing photos. The site (although extremely confusing to navigate if you don't read Cyrillic) is quite impressive; particularly the embedded videos on some of its pages. Some of the really interesting pages are this one on the Spiral "50/50" space fighter (in english) showing the interior, cargo bay, and weapons set-up: http://www.buran.ru/htm/str126.htm The MiG-105 Spiral testbed, with films of it in flight: http://www.buran.ru/htm/epos.htm And these two Buran pages that have clickable cutaways on them: http://www.buran.ru/htm/kompon.htm http://www.buran.ru/htm/konstr.htm Pat |
#86
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![]() John Doe ) writes: Andre Lieven wrote: ATV exists. It's not complete yet, and a year from flying roughly, but it exists. Until it flies, and flies successfully, I don't count it. Period. PR flyers are a dime a dozen. Flown systems are the real thing. ATV is more realistic than HTV, Klipper or CEV. They've already fitted the station with the gear to let its guidance system dock. The first flight ATV has been built. ATV has a lot of conventional technologies: MPLM shell for cargo module. Russian made docking module. Ariane 5 for launcher. But there is also a lot of new stuff (guidance, propulsion for orbiting tug etc). Has it flown ? No. My point. It is already late. And likely to see more delays while they debug the vehicle. And hopefully the modified Arianne 5 won't blow up when it launches ATV. So yes, you can't bet your life on ATV yet. But it is far from being vapourware. Ibid. HTV on the other hand is a big question mark. ESA has experience with Arianne 5. How much experience does Japan have with launchers ? Look it up for yourself. Andre -- " I'm a man... But, I can change... If I have to... I guess. " The Man Prayer, Red Green. |
#87
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![]() Quote:
http://www.esa.int/techresources/EST...386985867.html ATV will fly in 2006 (before june). You bet? Rémy |
#88
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John Doe wrote in :
"Jorge R. Frank" wrote: And you'll have to send replacements more frequently, since you'll have no real idea why they keep failing if you can't bring the failed ones back to the ground intact. The next step in space evolution would be to have the tools and documentation to allow the ISS crewmembers to perform the forensic analysys of failed components. (assuming CMGs could be fitted through airlock hatch, or at least a CMG with creative use of an empty MPLM with arm. Well, no... that's two or three steps away. The *next* step is to shift the design paradigm away from achieving reliability by means of redundancy at the system or subsystem level, and towards achieving reliability by redundancy at the component level. System and subsystem redundancy is fine for short trips but can be vulnerable to common-mode failures in the long term, and these types of vulnerabilities can be very hard to wring out during testing. That paradigm shift implies a different set of "virtues" for subsystem design: everything must be designed for crew servicing, and to the extent possible, subsystems should use a minimum number of common components. That in turn will minimize the number of tools and spare components that must be carried Only then, I believe, will onboard forensics be truly practical. -- JRF Reply-to address spam-proofed - to reply by E-mail, check "Organization" (I am not assimilated) and think one step ahead of IBM. |
#90
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On Mon, 22 Aug 2005 18:50:13 -0500, Chris J. wrote
(in article ): Wasn't one of the early claims regarding it's modular design that older modules could be replaced with newer ones? Only theoretically; it was never seriously planned given the cost of designing and building the first set of modules (costs NASA and the contractor team realized all along would preclude it in actuality). I may be in error, but I thought I recalled that from when the project was in it's proposal stages. I take it that is no longer the case, if it ever was? I don't doubt NASA let people believe that it was a possibility - the reality is that neither ISS nor SSF before it was ever planned to remove and replace modules. The modules themselves and all equipment inside them were originally spec'd for 30 year on-orbit operational lifetimes. This was decreased fo 15 years following the SSF CDR in 1993, mostly as a way to reduced projected final dev and qaul costs and due to a grudging realization by NASA that a 30 year life was going to cost way in excess of a 15 year life. -- "Fame may be fleeting but obscurity is forever." ~Anonymous "I believe as little as possible and know as much as I can." ~Todd Stuart Phillips www.angryherb.net |
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