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GSLV-3
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Gross Mass: 14,600 kg (32,100 lb). Empty Mass: 2,200 kg (4,800 lb). Thrust (vac): 75.050 kN (16,872 lbf). Isp: 460 sec. Burn time: 675 sec. Propellants: Lox/LH2. Diameter: 2.80 m (9.10 ft). Span: 2.80 m (9.10 ft). Length: 8.72 m (28.60 ft). Country: India. No Engines: 1. Engine: RD-56M. Status: In production. First Flight: 2001. Last Flight: 2006. No Launched: 4. Other designations: Geostationary Satellite Launch Vehicle.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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