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Engine Model: RH-300. Designer: ISRO. Gross Mass: 300 kg (660 lb). Empty Mass: 79 kg (174 lb). Propellants: Solid. Thrust(vac): 33.300 kN (7,486 lbf). Burn time: 16 sec. Diameter: 0.31 m (1.01 ft). Length: 2.80 m (9.10 ft). Country: India.
Engine Model: RH-300-II. Designer: ISRO. Gross Mass: 500 kg (1,100 lb). Propellants: Solid. Thrust(vac): 39.100 kN (8,790 lbf). Burn time: 20 sec. Diameter: 0.31 m (1.01 ft). Length: 3.40 m (11.10 ft). Country: India.
RH-300 used on Rocket Stages - Used on stage: RH-300. on launch vehicle: RH.
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