SLV-4

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Model: SLV-4. Gross Mass: 360 kg (790 lb). Empty Mass: 98 kg (216 lb). Thrust (vac): 26.830 kN (6,032 lbf). Isp: 283 sec. Burn time: 33 sec. Propellants: Solid. Isp(sl): 60 sec. Diameter: 0.66 m (2.16 ft). Span: 0.66 m (2.16 ft). Length: 1.50 m (4.90 ft). Country: India. No Engines: 1. Motor: SLV-4. Status: Retired 1983. Cost $ : 0.500 million. First Flight: 1979. Last Flight: 1983. No Launched: 4. Other designations: Satellite Launch Vehicle. Model: ASLV-4. Gross Mass: 512 kg (1,128 lb). Empty Mass: 195 kg (429 lb). Thrust (vac): 34.999 kN (7,868 lbf). Isp: 281 sec. Burn time: 33 sec. Propellants: Solid. Isp(sl): 110 sec. Diameter: 0.66 m (2.16 ft). Span: 0.66 m (2.16 ft). Length: 1.40 m (4.50 ft). Country: India. No Engines: 1. Motor: SLV-4. Status: Retired 1994. Cost $ : 0.500 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.