This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 25,200 kg.
Empty Mass: 2,355 kg. Thrust (vac): 30,000 kgf. Isp: 359 sec. Burn time: 300 sec. Propellants: Lox/Kerosene Diameter: 2.7 m. Span: 2.7 m. Length: 6.7 m. Country: Russia. No Engines: 1. RD-0124 Status: Development. Comments: Two thrust levels. Propellant ration 2.6:1, chamber pressure 162 bar.
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Last update 12 March 2001.
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© Mark Wade, 2001 .