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MRM-106
Part of MR-100 engine series
MRM-106B
MRM-106B
Credit: Aerojet Redmond
Redmond Hydrazine rocket engine. In Production. Steady-state thrust 9 N.

Status: In Production. Thrust: 27 N (6 lbf). Unfuelled mass: 0.94 kg (2.07 lb). Specific impulse: 231 s. Burn time: 2,991 s. Height: 0.17 m (0.56 ft). Diameter: 0.0310 m (0.1010 ft).

Engine: 0.94 kg (2.07 lb). Restarts: 1570.

Family: Storable liquid. Country: USA. Agency: Redmond.
Photo Gallery
MRM-106CMRM-106C
Credit: Aerojet Redmond
MRM-106DMRM-106D
Credit: Aerojet Redmond
MRM-106EMRM-106E
Credit: Aerojet Redmond
MRM-106FMRM-106F
Credit: Aerojet Redmond
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