The Story of Baikonur, Russia's Space City 237
eldavojohn writes "There's an article up on Physorg about Russian space launch city Baikonur, rented by Russia from Kazakhstan. Although it is essentially the same as it was in the 60's and 70's, it is amazingly efficient and still operational. 'Even the technology hasn't changed much. The Soyuz spacecraft designed in the mid-1960s is still in service, somewhat modified. It can only be used once, but costs just $25 million. The newest Endeavor space shuttle cost $2 billion, but is reusable. Life and work in Baikonur and its cosmodrome are also pretty much what they were in the Soviet era. The town of 70,000 - unbearably hot in summer, freezing cold in winter and dusty year round - is isolated by hundreds of miles of scrubland.'" We last discussed Baikonur back in 2005.
Costs (Score:5, Informative)
It also lists the launch costs for a shuttle at about $450 million. I don't know if that's just the launch itself or if that includes the turn around costs. Of course - the article doesn't list similar numbers for the Soyuz - but it seems that while reusable - the shuttle still is exponentially more expensive. Although - I don't know of anything else that can get as much weight to orbit as the shuttle.
Re:Costs (Score:5, Informative)
At 21,000 kg to LEO, the Ariane 5 ECA [wikipedia.org] comes pretty close. And it does a lot better than the shuttle [wikipedia.org] to Geostationary Transfer Orbit. The Delta IV [wikipedia.org] does slightly better than the shuttle at 25,800kg to LEO versus the shuttle's 24,400kg.
The Saturn V [wikipedia.org] could put them all to shame. Although the planned Ares V [wikipedia.org] can carry even more than the Saturn V.
Re:Costs (Score:3, Informative)
Baikonur - Kazakhstan vs. Russia (Score:2, Informative)
See this article from EurasiaNet: http://eurasianet.org/resource/kazakhstan/hypermail/news/0011.shtml [eurasianet.org]
Re:Bargain space flight (Score:5, Informative)
They did bring 2 or 3 Sats down from orbit in the early days
Re:Reusable shuttle? Not really .. (Score:5, Informative)
Re:Costs (Score:2, Informative)
and
Re:Costs (Score:5, Informative)
The launcher can lift 7,800 kg to LEO.
Re:Costs (Score:1, Informative)
Re:Costs (Score:3, Informative)
Saturn V lifted 118,000kg to LEO, Ares V will be 130,000kg to LEO. The shuttle is a mere 24,400kg to LEO (discounting the mass of the shuttle orbiter, itself).
All would've been outperformed by a maximum-configuration Energia-Vulkan @ 175,000kg to LEO. Frankly, nobody's ever come up with anything like a big enough rocket to really put human spaceflight into gear (i.e. Putting supplies & 20-50 people up, at once). You'd be looking in the range in excess of one kiloton to LEO, for this (i.e. Lifting a mass equivalent to twice the ISS, simultaneously). Just for an idea of scale, this would make any rocket about eight times more massive than a Saturn V, using present engine technology.
As has been pointed out elsewhere, Russian tech is excellent value & often to a higher standard than it's NASA equivalent. Energia-Vulkan would've put Ares V so shame, both on lifting ability &, no doubt, on cost too. A damned shame it was never fully developed, as it would've shown everyone the way forward. The price we pay for finishing off Communism, eh? However, it isn't as though NASA hasn't relied on Russian technology on their own rockets, in the past, either. The RD180 engine design was acquired pretty much straight from Energomash's RD170 & used on an Atlas rocket, just because it had a feedback mechanism to the engine, for unspent fuel, making the engine more efficient; something which NASA engineers hadn't even thought about.
Re:Don't believe the $25 million (Score:3, Informative)