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Engine Model: PSLV-1. Designer: ISRO. Gross Mass: 160,200 kg (353,100 lb). Empty Mass: 31,200 kg (68,700 lb). Propellants: Solid. Thrust(vac): 4,860.000 kN (1,092,570 lbf). Thrust(sl): 4,363.000 kN (980,841 lbf). Isp: 264 sec. Isp (sea level): 237 sec. Burn time: 97 sec. Diameter: 2.80 m (9.10 ft). Length: 20.34 m (66.73 ft). Chambers: 1. Chamber Pressure: 58.00 bar. Area Ratio: 8.00. Country: India. First Flight: 1993. Last Flight: 2006. Flown: 12.
PSLV-1 used on Rocket Stages
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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