This page no longer updated from 31 October 2001. Latest version can be found at R-36M2-3

Gross Mass: 8,200 kg. Empty Mass: 2,000 kg. Thrust (vac): 1,900 kgf. Isp: 317 sec. Burn time: 1,000 sec. Propellants: N2O4/UDMH Diameter: 3.0 m. Span: 3.0 m. Length: 1.0 m. Country: Ukraine. No Engines: 1. RD-869 Status: Hardware. Comments: Empty mass estimated.
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Last update 12 March 2001.
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© Mark Wade, 2001 .