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Soyuz 11A511-1
Part of R-7 Block A stage series
LOx/Kerosene propellant rocket stage. .

AKA: 11S59 Block D. Status: Retired 1975. Thrust: 977.70 kN (219,796 lbf). Gross mass: 100,500 kg (221,500 lb). Unfuelled mass: 6,500 kg (14,300 lb). Specific impulse: 315 s. Specific impulse sea level: 252 s. Burn time: 292 s. Height: 27.80 m (91.20 ft). Diameter: 2.95 m (9.67 ft). Span: 2.95 m (9.67 ft).

Cost $ : 13.000 million.



Country: Russia. Engines: RD-108-11D512. Launch Vehicles: Soyuz 11A511, Soyuz 11A510. Propellants: Lox/Kerosene.

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