RM-1100

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Engine Model: RM-1100. Designer: Cooper. Gross Mass: 100 kg (220 lb). Empty Mass: 18 kg (39 lb). Propellants: Solid. Thrust(vac): 26.000 kN (5,845 lbf). Burn time: 5.30 sec. Diameter: 0.17 m (0.54 ft). Length: 2.70 m (8.80 ft). Country: USA. RM-1100 used on Rocket Stages Used on stage: Asp. on launch vehicle: Asp. Used on stage: Asp. on launch vehicle: Astrobee. Used on stage: Asp. on launch vehicle: Loki. Used on stage: Asp. on launch vehicle: Rockoon. Used on stage: Asp. on launch vehicle: Terrier. 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.