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Vostok 8A92M-0
Part of R-7 Block BVGD stage series Family
LOx/Kerosene propellant rocket stage. .

Status: Retired 1991. Thrust: 995.30 kN (223,752 lbf). Gross mass: 43,300 kg (95,400 lb). Unfuelled mass: 3,700 kg (8,100 lb). Specific impulse: 313 s. Specific impulse sea level: 256 s. Burn time: 120 s. Height: 19.00 m (62.00 ft). Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft).

Cost $ : 5.000 million.

Country: Russia. Engines: RD-107-8D74K. Launch Vehicles: Vostok 8A92M. Propellants: Lox/Kerosene.



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