This page no longer updated from 31 October 2001. Latest version can be found at SLV-3

Designer: ISRO. Used on stages: ASLV-3, SLV-3. Used on launch vehicles: ASLV, SLV. Gross Mass: 1,500 kg. Empty Mass: 440 kg. Propellants: Solid Thrust(vac): 9,249 kgf. Thrust(vac): 90.70 kN. Isp: 277 sec. Isp (sea level): 190 sec. Burn time: 45 sec. Diameter: 0.8 m. Length: 2.3 m. Chambers: 1. Chamber Pressure: 43.00 bar. Area Ratio: 24.00. Country: India. Status: In Production. First Flight: 1979. Last Flight: 1994. Flown: 8.
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Last update 12 March 2001.
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© Mark Wade, 2001 .