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Soyuz 11A511U-0
Part of R-7 Block BVGD stage series Family
LOx/Kerosene propellant rocket stage. Gross mass includes 1190 kg of hydrogen peroxide and 280 kg of liquid nitrogen expended during ascent but not contributing to propulsion.

Status: Design 2000. Thrust: 994.30 kN (223,528 lbf). Gross mass: 44,500 kg (98,100 lb). Unfuelled mass: 3,784 kg (8,342 lb). Specific impulse: 310 s. Specific impulse sea level: 264 s. Burn time: 120 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 11A511U / Ikar, Soyuz 11A511U / Fregat. Propellants: Lox/Kerosene.

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