SLV-2

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Model: SLV-2. Gross Mass: 4,900 kg (10,800 lb). Empty Mass: 1,750 kg (3,850 lb). Thrust (vac): 267.005 kN (60,025 lbf). Isp: 267 sec. Burn time: 40 sec. Propellants: Solid. Isp(sl): 216 sec. Diameter: 0.80 m (2.62 ft). Span: 0.80 m (2.62 ft). Length: 6.35 m (20.83 ft). Country: India. No Engines: 1. Motor: SLV-2. Status: Retired 1983. Cost $ : 1.500 million. First Flight: 1979. Last Flight: 1983. No Launched: 4. No Failed: 1. Other designations: Satellite Launch Vehicle. Model: ASLV-2. Gross Mass: 4,400 kg (9,700 lb). Empty Mass: 800 kg (1,760 lb). Thrust (vac): 304.000 kN (68,341 lbf). Isp: 276 sec. Burn time: 36 sec. Propellants: Solid. Isp(sl): 220 sec. Diameter: 0.80 m (2.62 ft). Span: 0.80 m (2.62 ft). Length: 6.35 m (20.83 ft). Country: India. No Engines: 1. Motor: SLV-2. Status: Retired 1994. Cost $ : 1.500 million. First Flight: 1987. Last Flight: 1994. No Launched: 4. Other designations: Advanced Satellite Launch Vehicle. Used on Launch Vehicles: ASLV. SLV. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.