This page no longer updated from 31 October 2001. Latest version can be found at R-36-0-2

Gross Mass: 48,000 kg. Empty Mass: 5,000 kg. Thrust (vac): 97,484 kgf. Isp: 317 sec. Burn time: 160 sec. Propellants: N2O4/UDMH Diameter: 3.0 m. Span: 3.0 m. Length: 9.4 m. Country: Ukraine. No Engines: 1. RD-252 Status: Hardware.
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Last update 12 March 2001.
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© Mark Wade, 2001 .