Description
MR-501 0.09N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 0.60 kg, with a specific impulse of 180 to 184 sec (steady state) and a thrust of 0.07 to 0.09 N (steady state).
MR-501 0.09N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 0.60 kg, with a specific impulse of 180 to 184 sec (steady state) and a thrust of 0.07 to 0.09 N (steady state).
Name | MR-401 0.09N |
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 | 0.6 kg |
Nominal Power | 11.95 W |