Description
MRM-106F 40N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 2.23 kg, with a specific impulse of 231 sec and a thrust of 40 N per rocket (steady state).
MRM-106F 40N
Aerojet Rocketdyne – MRM-106F 40NOverview
| Name | MRM-106F 40N |
| Manufacturer | Aerojet Rocketdyne |
| Subsystem | Propulsion |
| Classification | Monoprop Thruster |
| Form Factor | SmallSat |
| TRL | 9 |
| Heritage | Yes |
Vendor Overview
| Vendor Name | Aerojet Rocketdyne |
| Vendor Website | https://www.rocket.com |
| Vendor Location | United States |
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SPECIFICATIONS
| Subsystem | Propulsion |
| Classification | Monoprop Thruster |
| Form Factor | SmallSat |
| Vendor | Aerojet Rocketdyne |
| Heritage | Yes |
| Mass | 2.23 kg |
| Nominal Power | 20.1 W |
