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Sputnik 8A91-1
Part of R-7 Block A stage series Family
LOx/Kerosene propellant rocket stage. .

Status: Out of Production. Thrust: 804.00 kN (180,746 lbf). Gross mass: 95,000 kg (209,000 lb). Unfuelled mass: 7,100 kg (15,600 lb). Specific impulse: 315 s. Specific impulse sea level: 246 s. Burn time: 360 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-108-8D77. Propellants: Lox/Kerosene.

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