Soyuz 11A511-0 (original) (raw)

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Soyuz 11A511-0

Part of R-7 Block BVGD stage series

LOx/Kerosene propellant rocket stage. .

AKA: 11S59 Blocks A,B,V,G. Status: Retired 1975. Thrust: 994.30 kN (223,528 lbf). Gross mass: 43,000 kg (94,000 lb). Unfuelled mass: 3,550 kg (7,820 lb). Specific impulse: 314 s. Specific impulse sea level: 257 s. Burn time: 118 s. Height: 19.60 m (64.30 ft). Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft).

Cost $ : 5.000 million.

Country: Russia. Engines: RD-107-11D511. Launch Vehicles: Soyuz 11A511, Soyuz 11A510. Propellants: Lox/Kerosene.

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