This page no longer updated from 31 October 2001. Latest version can be found at SLV-4

Designer: ISRO. Used on stages: ASLV-4, SLV-4. Used on launch vehicles: ASLV, SLV. Gross Mass: 360 kg. Empty Mass: 98 kg. Propellants: Solid Thrust(vac): 2,736 kgf. Thrust(vac): 26.80 kN. Isp: 283 sec. Isp (sea level): 60 sec. Burn time: 33 sec. Diameter: 0.7 m. Length: 1.5 m. Chambers: 1. Chamber Pressure: 29.00 bar. Area Ratio: 31.00. 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 .