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PSLV-1
ISRO solid rocket engine. Used on GSLV, PSLV. First flight 1993. GSLV first stage.

AKA: GSLV-1. Status: Active. Number: 12 . Thrust: 4,860.00 kN (1,092,570 lbf). Gross mass: 160,200 kg (353,100 lb). Unfuelled mass: 31,200 kg (68,700 lb). Specific impulse: 264 s. Specific impulse sea level: 237 s. Burn time: 97 s. Height: 20.34 m (66.73 ft). Diameter: 2.80 m (9.10 ft).

Thrust (sl): 4,363.000 kN (980,841 lbf). Thrust (sl): 444,905 kgf. Chamber Pressure: 58.00 bar. Area Ratio: 8.



Country: India. Launch Vehicles: PSLV, GSLV, PSLV C. Propellants: Solid. Stages: PSLV-1. Agency: ISRO.

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