This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 3,210,000 kg.
Empty Mass: 222,100 kg. Thrust (vac): 4,116,000 kgf. Isp: 322 sec. Burn time: 151 sec. Propellants: N2O4/UDMH Isp(sl): 301 sec. Diameter: 17.6 m. Span: 24.9 m. Length: 53.6 m. Country: Russia. No Engines: 6. RD-270 Status: Development 1967. Comments: Includes propellant tanks which fed stage two engines from liftoff to first stage cutoff.
Back to Index
Last update 12 March 2001.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .