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SLV-3 engine
Part of SLV-2 Family
ISRO solid rocket engine. Used on ASLV, SLV. First flight 1979. ASLV third stage.

AKA: ASLV-3;SLV-3. Status: Retired 1983. Number: 8 . Thrust: 90.70 kN (20,390 lbf). Gross mass: 1,500 kg (3,300 lb). Unfuelled mass: 440 kg (970 lb). Specific impulse: 277 s. Specific impulse sea level: 190 s. Burn time: 45 s. Height: 2.30 m (7.50 ft). Diameter: 0.82 m (2.69 ft).

Thrust (sl): 62.200 kN (13,983 lbf). Thrust (sl): 6,344 kgf. Chamber Pressure: 43.00 bar. Area Ratio: 24.



Country: India. Launch Vehicles: SLV, SLV-3 D4, SLV-3, ASLV. Propellants: Solid. Stages: SLV-3 engine. Agency: ISRO.

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