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Gross Mass: 5,250,000 kg (11,570,000 lb). Empty Mass: 500,000 kg (1,100,000 lb). Thrust (vac): 102,013.600 kN (22,933,570 lbf). Isp: 337 sec. Burn time: 200 sec. Propellants: Lox/Kerosene. Isp(sl): 311 sec. Diameter: 12.50 m (41.00 ft). Span: 30.50 m (100.00 ft). Length: 30.00 m (98.00 ft). Country: Russia. No Engines: 16. 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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