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UR-700M-2
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: 102,013.60 kN (22,933,570 lbf). Gross mass: 5,250,000 kg (11,570,000 lb). Unfuelled mass: 500,000 kg (1,100,000 lb). Specific impulse: 337 s. Specific impulse sea level: 311 s. Burn time: 200 s. Height: 30.00 m (98.00 ft). Diameter: 12.50 m (41.00 ft). Span: 30.50 m (100.00 ft).

No Engines: 16.



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

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