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Sputnik 8K71PS-1
Part of R-7 Block A stage series Family
LOx/Kerosene propellant rocket stage. .

Status: Retired 1957. Thrust: 912.00 kN (205,025 lbf). Gross mass: 94,000 kg (207,000 lb). Unfuelled mass: 7,495 kg (16,523 lb). Specific impulse: 308 s. Specific impulse sea level: 241 s. Burn time: 310 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-108-8D75PS. Launch Vehicles: Sputnik 8K71PS. Propellants: Lox/Kerosene.

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