This page no longer updated from 31 October 2001.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

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.
Back to Index
Last update 12 March 2001.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .