This page no longer updated from 31 October 2001.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

Designer: ISRO. Used on stages: PSLV-4. Used on launch vehicles: PSLV. Propellants: N2O4/MMH Thrust(vac): 714 kgf. Thrust(vac): 7.00 kN. Isp: 308 sec. Burn time: 425 sec. Diameter: 0.7 m. Chambers: 1. Chamber Pressure: 8.40 bar. Area Ratio: 60.00. Thrust to Weight Ratio: 0.00. Country: India. Status: In Production. First Flight: 1993. Last Flight: 1997. Flown: 8.
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Last update 12 March 2001.
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© Mark Wade, 2001 .