Russian heavy-lift orbital launch vehicle. UR-700 with high energy upper stage consisting of 3 x RD-350 LF2/LH2 engines with a total thrust of 450 tonnes. Usable third stage propellant 350 tonnes, payload increased to 215 tonnes
LEO Payload: 215,000 kg (473,000 lb) to a 200 km orbit at 51.00 degrees.
Status: Design 1968.
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Gross mass: 4,800,000 kg (10,500,000 lb).
Payload: 215,000 kg (473,000 lb).
Height: 76.00 m (249.00 ft).
Diameter: 17.60 m (57.70 ft).
Thrust: 56,500.00 kN (12,701,700 lbf).
Apogee: 200 km (120 mi).
UR-700 The UR-700 was the member of Vladimir Chelomei's Universal Rocket family designed in the 1960's to allow direct manned flight by the LK-700 spacecraft to the surface of the moon. Later versions, some of completely different configuration, were studied for manned Mars expeditions. More...
Associated Manufacturers and Agencies
Chelomei Russian manufacturer of rockets, spacecraft, and rocket engines. Chelomei Design Bureau, Reutov, Russia. More...
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