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RH-300 engine
ISRO solid rocket engine. RH-300 first stage.

AKA: RH-300;RH-300-1. Status: Retired 1993. Number: 1 . Thrust: 33.30 kN (7,486 lbf). Gross mass: 300 kg (660 lb). Unfuelled mass: 79 kg (174 lb). Burn time: 16 s. Height: 2.80 m (9.10 ft). Diameter: 0.31 m (1.01 ft).

Country: India. Launch Vehicles: RH-560, RH-300, RH-300 TV. Propellants: Solid. Stages: RH-300 engine. Agency: ISRO.
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