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R-7A 8K74-0


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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 R-7A 8K74-0 Part of R-7 Block BVGD stage series LOx/Kerosene propellant rocket stage. .

Status: Retired 1967. Thrust: 995.30 kN (223,752 lbf). Gross mass: 42,800 kg (94,300 lb). Unfuelled mass: 3,200 kg (7,000 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: R-7A. 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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