RH-200

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Model: RH-200-1. Gross Mass: 100 kg (220 lb). Thrust (vac): 16.900 kN (3,799 lbf). Burn time: 5.70 sec. Propellants: Solid. Diameter: 0.20 m (0.65 ft). Length: 1.40 m (4.50 ft). Country: India. No Engines: 1. Motor: RH-200. Status: Active. First Flight: 1979. Last Flight: 2008. No Launched: 805. Used as: RH-200. Release conditions: ISRO. Used on Launch Vehicles: RH. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.