This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
astronautix.com Sputnik 8A91-0
R-7 aft end
R-7 aft end -

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

Gross Mass: 43,000 kg. Empty Mass: 3,400 kg. Thrust (vac): 99,000 kgf. Isp: 310 sec. Burn time: 130 sec. Propellants: Lox/Kerosene Isp(sl): 252 sec. Diameter: 2.7 m. Span: 2.7 m. Length: 19.0 m. Country: Russia. No Engines: 1. RD-107-8D76 Status: Hardware.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .