| RH-300 |
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Model: RH-300-1. Gross Mass: 300 kg (660 lb). Empty Mass: 79 kg (174 lb). Thrust (vac): 33.300 kN (7,486 lbf). Burn time: 16 sec. Propellants: Solid. Diameter: 0.31 m (1.01 ft). Length: 2.80 m (9.10 ft). Country: India. No Engines: 1. Motor: RH-300. Status: Retired 1993. First Flight: 1974. Last Flight: 1993. No Launched: 19. Used as: Belier. Release conditions: ISRO.
Model: RH-300 Mk II-1. Gross Mass: 500 kg (1,100 lb). Thrust (vac): 39.100 kN (8,790 lbf). Burn time: 20 sec. Propellants: Solid. Diameter: 0.31 m (1.01 ft). Length: 3.40 m (11.10 ft). Country: India. No Engines: 1. Motor: RH-300-II. Status: Active. First Flight: 1987. Last Flight: 2005. No Launched: 13. Used as: Belier. Release conditions: ISRO.
Used on Launch Vehicles:
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