SLV-3

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Model: SLV-3. Gross Mass: 1,500 kg (3,300 lb). Empty Mass: 440 kg (970 lb). Thrust (vac): 90.701 kN (20,390 lbf). Isp: 277 sec. Burn time: 45 sec. Propellants: Solid. Isp(sl): 190 sec. Diameter: 0.82 m (2.69 ft). Span: 0.82 m (2.69 ft). Length: 2.30 m (7.50 ft). Country: India. No Engines: 1. Motor: SLV-3. Status: Retired 1983. Cost $ : 1.000 million. First Flight: 1979. Last Flight: 1983. No Launched: 4. Other designations: Satellite Launch Vehicle. Model: ASLV-3. Gross Mass: 1,710 kg (3,760 lb). Empty Mass: 650 kg (1,430 lb). Thrust (vac): 90.701 kN (20,390 lbf). Isp: 277 sec. Burn time: 45 sec. Propellants: Solid. Isp(sl): 190 sec. Diameter: 0.82 m (2.69 ft). Span: 0.82 m (2.69 ft). Length: 2.44 m (8.00 ft). Country: India. No Engines: 1. Motor: SLV-3. Status: Retired 1994. Cost $ : 1.000 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.