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R-7 8K71-1
Part of R-7 Block A stage series
LOx/Kerosene propellant rocket stage. .

Status: Retired 1961. Thrust: 912.00 kN (205,025 lbf). Gross mass: 95,300 kg (210,100 lb). Unfuelled mass: 7,500 kg (16,500 lb). Specific impulse: 308 s. Specific impulse sea level: 241 s. Burn time: 330 s. Height: 28.00 m (91.00 ft). Diameter: 2.99 m (9.80 ft). Span: 2.99 m (9.80 ft).

Cost $ : 13.000 million.



Country: Russia. Engines: RD-108-8D75. Launch Vehicles: R-7. Propellants: Lox/Kerosene.

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