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Soyuz 11A511U2-1
Part of R-7 Block A stage series Family
LOx/Kerosene propellant rocket stage. .

Status: Retired 1996. Thrust: 1,011.00 kN (227,281 lbf). Gross mass: 101,160 kg (223,010 lb). Unfuelled mass: 6,500 kg (14,300 lb). Specific impulse: 319 s. Specific impulse sea level: 252 s. Burn time: 286 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-108-11D512P. Launch Vehicles: Soyuz-U2. Propellants: Lox/Kerosene.

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