RM-1400

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Engine Model: RM-1400. Designer: Cooper. Gross Mass: 94 kg (207 lb). Empty Mass: 27 kg (59 lb). Propellants: Solid. Thrust(vac): 12.700 kN (2,855 lbf). Burn time: 12 sec. Diameter: 0.17 m (0.54 ft). Length: 2.80 m (9.10 ft). Country: USA. RM-1400 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.