RH-560

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Engine Model: RH-560. Designer: ISRO/Antrix. Gross Mass: 900 kg (1,980 lb). Empty Mass: 277 kg (610 lb). Propellants: Solid. Thrust(vac): 76.000 kN (17,085 lbf). Burn time: 19 sec. Diameter: 0.56 m (1.83 ft). Length: 3.90 m (12.70 ft). Country: India. RH-560 used on Rocket Stages Used on stage: RH-560. 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.