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UR-700M-1
LOx/Kerosene propellant rocket stage. Total mass, length, estimated based on empty mass, total vehicle mass. Engine specific impulse estimated based on follow-on RD-170 engines.

Status: Design 1972. Thrust: 204,027.00 kN (45,867,094 lbf). Gross mass: 8,000,000 kg (17,600,000 lb). Unfuelled mass: 750,000 kg (1,650,000 lb). Specific impulse: 337 s. Specific impulse sea level: 311 s. Burn time: 115 s. Height: 35.00 m (114.00 ft). Diameter: 9.00 m (29.50 ft). Span: 30.50 m (100.00 ft).

No Engines: 32.



Country: Russia. Engines: RLA-300, RLA-600. Launch Vehicles: UR-700M. Propellants: Lox/Kerosene.

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