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SLV-4
ISRO solid rocket engine. Used on ASLV, SLV. First flight 1979. ASLV fourth stage.

AKA: ASLV-4. Status: Retired 1983. Number: 8 . Thrust: 26.80 kN (6,025 lbf). Gross mass: 360 kg (790 lb). Unfuelled mass: 98 kg (216 lb). Specific impulse: 283 s. Specific impulse sea level: 60 s. Burn time: 33 s. Height: 1.50 m (4.90 ft). Diameter: 0.66 m (2.16 ft).

Thrust (sl): 5.690 kN (1,279 lbf). Thrust (sl): 580 kgf. Chamber Pressure: 29.00 bar. Area Ratio: 31.



Country: India. Launch Vehicles: SLV, SLV-3 D4, SLV-3, ASLV. Propellants: Solid. Stages: SLV-4. Agency: ISRO.

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