RH-200

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Engine Model: RH-200. Designer: ISRO. Gross Mass: 100 kg (220 lb). Propellants: Solid. Thrust(vac): 16.900 kN (3,799 lbf). Burn time: 5.70 sec. Diameter: 0.20 m (0.65 ft). Length: 1.40 m (4.50 ft). Country: India. RH-200 used on Rocket Stages Used on stage: RH-200. on launch vehicle: 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.