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-401 0.09N
Aerojet Rocketdyne – MR-401 0.09NOverview
| Name | MR-401 0.09N |
| 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 | 0.6 kg |
| Nominal Power | 11.95 W |
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