This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: ISRO. Used on stages: ASLV-2, SLV-2. Used on launch vehicles: ASLV, SLV. Gross Mass: 4,900 kg. Empty Mass: 1,750 kg. Propellants: Solid Thrust(vac): 27,227 kgf. Thrust(vac): 267.00 kN. Isp: 267 sec. Isp (sea level): 216 sec. Burn time: 40 sec. Diameter: 0.8 m. Length: 6.4 m. Chambers: 1. Chamber Pressure: 43.00 bar. Area Ratio: 14.00. 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 .