This page no longer updated from 31 October 2001. Latest version can be found at Molniya M-3

Gross Mass: 4,500 kg. Empty Mass: 1,050 kg. Thrust (vac): 6,800 kgf. Isp: 340 sec. Burn time: 180 sec. Propellants: Lox/Kerosene Isp(sl): 0 sec. Diameter: 2.4 m. Span: 2.4 m. Length: 2.6 m. Country: Russia. No Engines: 1. Status: Hardware.
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Last update 12 March 2001.
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© Mark Wade, 2001 .