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Vostok 8A92M-2
Part of Block L Family
LOx/Kerosene propellant rocket stage. .

Status: Retired 1991. Thrust: 54.52 kN (12,257 lbf). Gross mass: 8,100 kg (17,800 lb). Unfuelled mass: 1,100 kg (2,400 lb). Specific impulse: 326 s. Burn time: 400 s. Height: 2.84 m (9.31 ft). Diameter: 2.56 m (8.39 ft). Span: 2.56 m (8.39 ft).

Cost $ : 3.000 million.



Country: Russia. Engines: RD-0109. Launch Vehicles: Vostok 8A92M. Propellants: Lox/Kerosene.

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