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Luna 8K72-1
Part of R-7 Block A stage series
LOx/Kerosene propellant rocket stage. .

Status: Retired 1960. Thrust: 936.50 kN (210,534 lbf). Gross mass: 95,300 kg (210,100 lb). Unfuelled mass: 6,900 kg (15,200 lb). Specific impulse: 315 s. Specific impulse sea level: 246 s. Burn time: 320 s. Height: 28.00 m (91.00 ft). Diameter: 2.60 m (8.50 ft). Span: 2.99 m (9.80 ft).

Cost $ : 13.000 million.



Country: Russia. Engines: RD-108-8D75-1958. Launch Vehicles: Vostok-L 8K72. Propellants: Lox/Kerosene.

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