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SLV-1
ISRO solid rocket engine. Used on ASLV, PSLV, SLV. First flight 1979.

AKA: ASLV-0;ASLV-1;PSLV-0. Status: Retired 1983. Number: 64 . Thrust: 502.60 kN (112,989 lbf). Gross mass: 10,800 kg (23,800 lb). Unfuelled mass: 2,140 kg (4,710 lb). Specific impulse: 253 s. Specific impulse sea level: 229 s. Burn time: 49 s. Height: 9.99 m (32.77 ft). Diameter: 1.00 m (3.20 ft).

Thrust (sl): 454.900 kN (102,266 lbf). Thrust (sl): 46,389 kgf. Chamber Pressure: 43.00 bar. Area Ratio: 6.7.



Subtopics

Agni St2 DRDO solid rocket engine. Agni 2 second stage.

Agni engine DRDO solid rocket engine. Agni 2 first stage.

Prithvi engine HAL solid rocket engine. Agni TD second stage.

Country: India. Launch Vehicles: SLV, SLV-3 D4, SLV-3, ASLV, PSLV, PSLV C. Propellants: Solid. Stages: SLV-1. Agency: ISRO.

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