
MRM-106B
Credit: Aerojet Redmond

MRM-106C
Credit: Aerojet Redmond

MRM-106D
Credit: Aerojet Redmond

MRM-106E
Credit: Aerojet Redmond

MRM-106F
Credit: Aerojet Redmond
Redmond Hydrazine rocket engine. 0.027 kN. In Production. Steady-state thrust 9 N. Isp=231s.
Engine: 0.94 kg (2.07 lb). Restarts: 1570.
Status: In Production.
Unfuelled mass: 0.94 kg (2.07 lb).
Height: 0.17 m (0.56 ft).
Diameter: 0.0310 m (0.1010 ft).
Thrust: 27 N (6 lbf).
Specific impulse: 231 s.
Burn time: 2,991 s.
More... - Chronology...
Associated Countries
See also
Associated Manufacturers and Agencies
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Redmond American manufacturer of rocket engines. Redmond, USA. More...
Associated Propellants
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Hydrazine Hydrazine (N2H4) found early use as a fuel, but it was quickly replaced by UDMH. It is still used as a monopropellant for satellite station-keeping motors. Hydrazine (N2H4) found early use as a fuel, but it was quickly replaced by UDMH. It is still used as a monopropellant for satellite station-keeping motors. More...
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