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UR-700M-3
LOx/LH2 propellant rocket stage. Total mass, length, estimated based on empty mass, total vehicle mass. Engine specific impulse estimated based on performance requirements.

Status: Design 1972. Thrust: 11,700.00 kN (2,630,200 lbf). Gross mass: 2,000,000 kg (4,400,000 lb). Unfuelled mass: 200,000 kg (440,000 lb). Specific impulse: 455 s. Burn time: 670 s. Height: 16.00 m (52.00 ft). Diameter: 12.50 m (41.00 ft). Span: 12.50 m (41.00 ft).

No Engines: 6.



Country: Russia. Engines: NK-15VM, NK-35. Launch Vehicles: UR-700M. Propellants: Lox/LH2.

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