UR-700 / RD-350

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UR-700 / RD-350

Part of UR-700

UR-700

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 metric tons. Usable third stage propellant 350 metric tons, payload increased to 215 metric tons

Status: Design 1968. Payload: 215,000 kg (473,000 lb). Thrust: 56,500.00 kN (12,701,700 lbf). Gross mass: 4,800,000 kg (10,500,000 lb). Height: 76.00 m (249.00 ft). Diameter: 17.60 m (57.70 ft). Apogee: 200 km (120 mi).

LEO Payload: 215,000 kg (473,000 lb) to a 200 km orbit at 51.00 degrees.

Family: heavy-lift, orbital launch vehicle. Country: Russia. Agency: Chelomei bureau.

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