| SLV-1 |
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Model: SLV-1. Gross Mass: 10,800 kg (23,800 lb). Empty Mass: 2,140 kg (4,710 lb). Thrust (vac): 502.600 kN (112,989 lbf). Isp: 253 sec. Burn time: 49 sec. Propellants: Solid. Isp(sl): 229 sec. Diameter: 1.00 m (3.20 ft). Span: 1.00 m (3.20 ft). Length: 9.99 m (32.77 ft). Country: India. No Engines: 1. Motor: SLV-1. Status: Retired 1983. Cost $ : 2.000 million. First Flight: 1979. Last Flight: 1983. No Launched: 4. Other designations: Satellite Launch Vehicle.
Model: ASLV-0. Gross Mass: 11,600 kg (25,500 lb). Empty Mass: 2,963 kg (6,532 lb). Thrust (vac): 502.600 kN (112,989 lbf). Isp: 253 sec. Burn time: 49 sec. Propellants: Solid. Isp(sl): 229 sec. Diameter: 1.00 m (3.20 ft). Span: 1.00 m (3.20 ft). Length: 9.99 m (32.77 ft). Country: India. No Engines: 1. Motor: SLV-1. Status: Retired 1994. Cost $ : 2.000 million. First Flight: 1987. Last Flight: 1994. No Launched: 8. Other designations: Advanced Satellite Launch Vehicle.
Model: ASLV-1. Gross Mass: 11,800 kg (26,000 lb). Empty Mass: 2,900 kg (6,300 lb). Thrust (vac): 702.009 kN (157,818 lbf). Isp: 259 sec. Burn time: 45 sec. Propellants: Solid. Isp(sl): 232 sec. Diameter: 1.00 m (3.20 ft). Span: 1.00 m (3.20 ft). Length: 9.99 m (32.77 ft). Country: India. No Engines: 1. Motor: SLV-1. Status: Retired 1994. Cost $ : 2.000 million. First Flight: 1987. Last Flight: 1994. No Launched: 4. Other designations: Advanced Satellite Launch Vehicle.
Model: PSLV-0. Gross Mass: 10,930 kg (24,090 lb). Empty Mass: 2,010 kg (4,430 lb). Thrust (vac): 502.600 kN (112,989 lbf). Isp: 262 sec. Burn time: 44 sec. Propellants: Solid. Isp(sl): 229 sec. Diameter: 1.00 m (3.20 ft). Span: 1.00 m (3.20 ft). Length: 9.99 m (32.77 ft). Country: India. No Engines: 1. Motor: SLV-1. Status: Active. Cost $ : 2.000 million. First Flight: 1993. Last Flight: 2007. No Launched: 120. Other designations: Polar Satellite Launch Vehicle.
Used on Launch Vehicles:
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