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Soyuz 11A511U2-2
Part of R-7 Block I stage series Family
LOx/Kerosene propellant rocket stage. .

Status: Retired 2007. Thrust: 298.10 kN (67,016 lbf). Gross mass: 25,400 kg (55,900 lb). Unfuelled mass: 2,400 kg (5,200 lb). Specific impulse: 330 s. Burn time: 250 s. Height: 6.74 m (22.11 ft). Diameter: 2.66 m (8.72 ft). Span: 2.66 m (8.72 ft).

Cost $ : 3.000 million.



Country: Russia. Engines: RD-0110. Launch Vehicles: Molniya 8K78M, Molniya 8K78M ML, Soyuz 11A511L, Soyuz 11A511M, Soyuz-U, Soyuz-U2, Molniya 8K78M SOL. Propellants: Lox/Kerosene.

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