[ol][li]Soviet Premier Leonid Brezhnev “bankrupted his country’s space program” is sometimes said, spent way more than was logical I would say, by launching what was the largest and the most expensive project in the history of the Soviet space exploration to build the Buran: maybe[/li][li]a copy of NASA’s space shuttle: wrong[/li][li]because some subset of his advisers persuaded him that the United States wanted to use the SHuttle for bombing from Space: wrong[/ol][/li]
All information from the k26 Group website, which is the most complete list of information about Buran and Energia I have found.[ul]
[li]Buran 1.01 (‘Buran’) was destroyed in the aforementioned hanger collapse[/li][li]Buran 1.02 (‘Ptichka’) is under possession of Kazakhstan, allegedly stored at Baikonur. It is, or at least was, the most completed of all orbiters (Buran never had any life support or cockpit controls installed, as the only flights it made were unmanned). Condition is unknown, but after 15+ years of presumably little maintenance it probably isn’t in flyable condition without rework. [/li][li]Buran 2.01 (unnamed) was 30-50% complete at the time of program cancellation, and was sold to an aviation museum in Sinsheim, Germany.[/li][li]Buran 2.02 (unnamed) was 10-20% complete at the time of program cancellation, and was left to rot at the Tushino Machine Building Plant just outside of Moscow. It appears to have been scavenged for parts for enthusiasts.[/li][li]Buran 2.03 (unnamed) was in an unknown state of construction at the time of program cancellation. It was dismantled.[/ul][/li]There were also a number of static and aerodynamic test models that were created as part of the development program. (Part of the reason that Buran cost so much more and took longer than STS was because it had a more extensive development and test program than NASA had for STS.) The k26 Group site has a partial list of test articles, but I believe that there were additional test models including several subscale aero/flight dynamics models.
There are no complete Buran airframes still in existance (though as noted above, Buran 1.02 was mostly complete and is allegedly mothballed, albeit in an uncertain state of maintenance and documentation). More importantly, while the S.P. Korolev Rocket and Space Corporation Energia (the commerical derivative of the government aerospace bureau which produced the Energya rocket) is still in existence, they haven’t built an Energya in almost two decades. It’s possible the the main tooling still exists in a usable state, but it seems likely, as with the Saturn V, that subcontractors and vendors (or the Soviet equivlent thereof) have gone out of business or lost documentation. Energia is still making rocket motors and boosters, including the Russian version of the RD-180 (a derivative of the RD-170 from the Zenit boosters) used on the Atlas III and Atlas V boosters and the R-7 heavy lift rocket for Soyuz/Progress. Energia is working on a new design called Angara which is a modular design which could (possibly) be scaled to boost Buran with minimal payload, but it seems unlikely that they could start cranking out Energya boosters again.
More to the point, why try to use Buran? Both American and Soviet experiences with heavy booster lifting body shuttles demonstrated that they are more expensive to operate than anticipated, and (at least with the STS) less reliable and more difficult to turn around than is acceptible. (Strictly speaking, the reliability of the American Shuttle is better, in terms of heads to orbit, than any other booster, and the major problems have been at least in part the paradoxical risk-adverse/risk-ignorant attitude of NASA, but nonetheless it failed to live up to even the modest and reduced goals expected of the final design.) The tendency after Challenger and the fall of the Soviet Union was to go to small, dedicated personnel lifting body shuttles and (now) capsules, and perform heavy lift operations via large unmanned boosters. This doesn’t allow for recovery and return of defective or malfunctioning satellites in orbit (one of the original mission requirements of the STS) but that turned out to be not cost effective anyway.
It’s probably cheaper–or at least it would be under a less bureaucratic organization than NASA and less money-grubbing contractors than the major aerospace/defense contenders for prime contract–and certainly safer to seperate personnel transport and heavy boost functions. The STS was mostly a justification for going to space and supporting Space Station Alpha/Freedom Station/the International Space Station, and the ISS has become the destination for the Shuttle now that it’s been firmly established that the STS cost to much for commercial launch and the Air Force doesn’t trust it from a risk standpoint.
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