This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Designer: ISRO. Used on stages: PSLV-3. Used on launch vehicles: PSLV. Gross Mass: 8,300 kg. Empty Mass: 1,100 kg. Propellants: Solid Thrust(vac): 33,519 kgf. Thrust(vac): 328.70 kN. Isp: 291 sec. Isp (sea level): 160 sec. Burn time: 75 sec. Diameter: 2.0 m. Length: 3.5 m. Chambers: 1. Chamber Pressure: 63.00 bar. Area Ratio: 52.00. Country: India. Status: In Production. First Flight: 1993. Last Flight: 1997. Flown: 4.
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Last update 12 March 2001.
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© Mark Wade, 2001 .