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RH-560 engine

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RH-560 engine
ISRO/Antrix solid rocket engine. RH-560B second stage.

AKA: RH-560; RH-560B-2. Status: Retired 1998. Number: 1 . Thrust: 76.00 kN (17,085 lbf). Gross mass: 900 kg (1,980 lb). Unfuelled mass: 277 kg (610 lb). Burn time: 19 s. Height: 3.90 m (12.70 ft). Diameter: 0.56 m (1.83 ft).

Country: India. Launch Vehicles: RH-560, RH-560/300 Mk II. Propellants: Solid. Stages: RH-560 engine. Agency: ISRO, Antrix.



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