This page no longer updated from 31 October 2001. Latest version can be found at Soyuz M-1

Gross Mass: 100,500 kg. Empty Mass: 6,000 kg. Thrust (vac): 89,000 kgf. Isp: 336 sec. Burn time: 310 sec. Propellants: Lox/Kerosene Isp(sl): 298 sec. Diameter: 3.0 m. Span: 3.0 m. Length: 28.0 m. Country: Russia. No Engines: 1. RD-120K Status: Development.
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 .