This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Gross Mass: 14,600 kg.
Empty Mass: 2,200 kg. Thrust (vac): 7,653 kgf. Isp: 460 sec. Burn time: 675 sec. Propellants: Lox/LH2 Diameter: 2.8 m. Span: 2.8 m. Length: 8.7 m. Country: India. No Engines: 1. RD-56M Status: Devel. Other designations: Geostationary Satellite Launch Vehicle.
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Last update 12 March 2001.
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© Mark Wade, 2001 .