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R-7 8K71-0
Part of R-7 Block BVGD stage series Family
LOx/Kerosene propellant rocket stage. .

Status: Retired 1961. Thrust: 970.00 kN (218,060 lbf). Gross mass: 43,100 kg (95,000 lb). Unfuelled mass: 3,500 kg (7,700 lb). Specific impulse: 306 s. Specific impulse sea level: 250 s. Burn time: 120 s. Height: 19.00 m (62.00 ft). Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft).

Cost $ : 5.000 million.



Country: Russia. Engines: RD-107-8D74. Launch Vehicles: R-7. Propellants: Lox/Kerosene.

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