Vostok 8K72-1 (original) (raw)

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Vostok 8K72-1

Part of R-7 Block A stage series

LOx/Kerosene propellant rocket stage. .

Status: Retired 1960. Thrust: 912.00 kN (205,025 lbf). Gross mass: 100,400 kg (221,300 lb). Unfuelled mass: 6,800 kg (14,900 lb). Specific impulse: 315 s. Specific impulse sea level: 246 s. Burn time: 310 s. Height: 28.00 m (91.00 ft). Diameter: 2.99 m (9.80 ft). Span: 2.99 m (9.80 ft).

Cost $ : 13.000 million.

Country: Russia. Engines: RD-108-8D75. Launch Vehicles: Vostok 8K72. Propellants: Lox/Kerosene.

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