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Luna 8K72-0


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A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z Luna 8K72-0 Part of R-7 Block BVGD stage series LOx/Kerosene propellant rocket stage. .

Status: Retired 1960. Thrust: 990.00 kN (222,560 lbf). Gross mass: 43,400 kg (95,600 lb). Unfuelled mass: 3,800 kg (8,300 lb). Specific impulse: 312 s. Specific impulse sea level: 254 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-107-8D74-1958. Launch Vehicles: Sputnik 8K71PS, Vostok-L 8K72. Propellants: Lox/Kerosene. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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