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Gross Mass: 8,000,000 kg (17,600,000 lb). Empty Mass: 750,000 kg (1,650,000 lb). Thrust (vac): 204,027.000 kN (45,867,094 lbf). Isp: 337 sec. Burn time: 115 sec. Propellants: Lox/Kerosene. Isp(sl): 311 sec. Diameter: 9.00 m (29.50 ft). Span: 30.50 m (100.00 ft). Length: 35.00 m (114.00 ft). Country: Russia. No Engines: 32. Engine: RLA-600. Status: Design 1972. Total mass, length, estimated based on empty mass, total vehicle mass. Engine specific impulse estimated based on follow-on RD-170 engines.
Used on Launch Vehicles:
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