This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com PSLV-3


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.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .