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PSLV-3
ISRO solid rocket engine. Used on PSLV launch vehicle. First flight 1993.

Status: Active. Number: 8 . Thrust: 328.70 kN (73,895 lbf). Gross mass: 8,300 kg (18,200 lb). Unfuelled mass: 1,100 kg (2,400 lb). Specific impulse: 291 s. Specific impulse sea level: 160 s. Burn time: 75 s. Height: 3.54 m (11.61 ft). Diameter: 1.99 m (6.52 ft).

Thrust (sl): 180.700 kN (40,623 lbf). Thrust (sl): 18,430 kgf. Chamber Pressure: 63.00 bar. Area Ratio: 52.



Subtopics

Agni3 S2 DRDO solid rocket engine. Agni 3 second stage.

Agni 3 engine DRDO solid rocket engine. Agni 3 first stage.

Country: India. Launch Vehicles: PSLV, PSLV C. Propellants: Solid. Stages: PSLV-3. Agency: ISRO.

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