RM-3141

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Engine Model: RM-3141. Designer: GCR. Gross Mass: 25 kg (55 lb). Empty Mass: 4.00 kg (8.80 lb). Propellants: Solid. Thrust(vac): 8.600 kN (1,933 lbf). Burn time: 7.60 sec. Diameter: 0.15 m (0.49 ft). Length: 1.20 m (3.90 ft). Country: USA. RM-3141 used on Rocket Stages Used on stage: Baby Sergeant. on launch vehicle: Asp. Used on stage: Baby Sergeant. on launch vehicle: Jaguar B-57. Used on stage: Baby Sergeant. on launch vehicle: Strongarm. 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.