MR-120 Redmond Hydrazine rocket engine. Small ICBM. In Production. Developed as an attitude control thruster for the small ICBM. |
MR-111 Redmond hydrazine monopropellant rocket engine. Attitude control, Intelsat 5, ERBS, ACTS, Radarsat, MMAS 4000, 5000, and. 7000, Wind/Polar Landsat, and Mars Observer. In Production. First flight 1980. |
MRM-122 Redmond Hydrazine rocket engine. In Production. Steady-state thrust 51 N. |
MR-103 Redmond hydrazine monopropellant rocket engine. Attitude control thruster for Voyager, GPS, Intelsat 5, MMAS 3000, 4000,. 5000, and 7000, Mars Observer, ACTS, and Magellan. In Production. First flight 1974. |
MRM-103 Redmond Hydrazine rocket engine. In Production. Steady-state thrust 0.22 N. |
MR-104 Redmond hydrazine monopropellant rocket engine. Attitude control and velocity corrections, Voyager, Magellan, DMSP, Tiros N, Landsat. In Production. First flight 1977. |
MR-106 Redmond hydrazine monopropellant rocket engine. Spacecraft and upper stage attitude control and velocity corrections, PAM A/S,. Radarsat, GPS Block 2R, HAS/Peace Courage, Titan Centaur, Atlas Centaur. In Production. |
MRM-106 Redmond Hydrazine rocket engine. In Production. Steady-state thrust 9 N. |
MR-107 Redmond hydrazine monopropellant rocket engine. Spacecraft and upper stage attitude control and dV corrections, Delta 2, Titan 2, PAM D, SICBM, HAS/Peace Courage, Atlas roll control module, STEP, Pegasus. First flight 1990. |