This page no longer updated from 31 October 2001. Latest version can be found at SLV-1

Designer: ISRO. Used on stages: ASLV-0, ASLV-1, PSLV-0, SLV-1. Used on launch vehicles: ASLV, PSLV, SLV. Gross Mass: 10,800 kg. Empty Mass: 2,140 kg. Propellants: Solid Thrust(vac): 51,251 kgf. Thrust(vac): 502.60 kN. Isp: 253 sec. Isp (sea level): 229 sec. Burn time: 49 sec. Diameter: 1.0 m. Length: 10.0 m. Chambers: 1. Chamber Pressure: 43.00 bar. Area Ratio: 6.70. Country: India. Status: In Production. First Flight: 1979. Last Flight: 1997. Flown: 40.
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Last update 12 March 2001.
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© Mark Wade, 2001 .