MR-125

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Engine Model: MR-125. Designer: LLNL. Gross Mass: 20 kg (44 lb). Empty Mass: 8.00 kg (17.60 lb). Propellants: Solid. Thrust(vac): 400 N (80 lbf). Burn time: 30 sec. Diameter: 0.17 m (0.55 ft). Length: 1.90 m (6.20 ft). Country: USA. MR-125 used on Rocket Stages Used on stage: Astrid. on launch vehicle: Astrid. 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.