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R-7 aft end
R-7 aft end -

Credit: © Mark Wade. 47,694 bytes. 421 x 583 pixels.

Gross Mass: 43,300 kg. Empty Mass: 3,710 kg. Thrust (vac): 99,000 kgf. Isp: 313 sec. Burn time: 118 sec. Propellants: Lox/Kerosene Isp(sl): 256 sec. Diameter: 2.7 m. Span: 2.7 m. Length: 19.0 m. Country: Russia. No Engines: 1. RD-107-8D74-1959 Status: Hardware.
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Last update 12 March 2001.
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© Mark Wade, 2001 .