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SLV-2
ISRO solid rocket engine. Used on ASLV, SLV. First flight 1979. ASLV second stage.

AKA: ASLV-2. Status: Retired 1983. Number: 8 . Thrust: 267.00 kN (60,023 lbf). Gross mass: 4,900 kg (10,800 lb). Unfuelled mass: 1,750 kg (3,850 lb). Specific impulse: 267 s. Specific impulse sea level: 216 s. Burn time: 40 s. Height: 6.35 m (20.83 ft). Diameter: 0.80 m (2.62 ft).

Thrust (sl): 216.000 kN (48,558 lbf). Thrust (sl): 22,026 kgf. Chamber Pressure: 43.00 bar. Area Ratio: 14.



Subtopics

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

Country: India. Launch Vehicles: SLV, SLV-3 D4, SLV-3, ASLV. Propellants: Solid. Stages: SLV-2. Agency: ISRO.

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