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 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).
Name | MRM-106F 40N |
Manufacturer | Aerojet Rocketdyne |
Subsystem | Propulsion |
Classification | Monoprop Thruster |
Form Factor | SmallSat |
TRL | 9 |
Heritage | Yes |
Vendor Name | Aerojet Rocketdyne |
Vendor Website | https://www.rocket.com |
Vendor Location | United States |
Subsystem | Propulsion |
Classification | Monoprop Thruster |
Form Factor | SmallSat |
Vendor | Aerojet Rocketdyne |
Heritage | Yes |
Mass | 2.23 kg |
Nominal Power | 20.1 W |