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Engine Model: PSLV-3. Designer: ISRO. Gross Mass: 8,300 kg (18,200 lb). Empty Mass: 1,100 kg (2,400 lb). Propellants: Solid. Thrust(vac): 328.700 kN (73,895 lbf). Thrust(sl): 180.700 kN (40,623 lbf). Isp: 291 sec. Isp (sea level): 160 sec. Burn time: 75 sec. Diameter: 1.99 m (6.52 ft). Length: 3.54 m (11.61 ft). Chambers: 1. Chamber Pressure: 63.00 bar. Area Ratio: 52.00. Country: India. First Flight: 1993. Last Flight: 2003. Flown: 8.00.
PSLV-3 used on Rocket Stages
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