MR-100 engine series
Original archive entry. The text, images and links below are kept as they were written.
Subtopics
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.