Description
MR-107V 300N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 1.01 kg (includes engine and valves), with a specific impulse of 223 to 229 sec and a thrust of 67 to 220 N (steady state).
MR-107V 300N
Aerojet Rocketdyne – MR-107V 300NOverview
| Name | MR-107V 300N |
| 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 | 1.01 kg |
| Nominal Power | 52.0 W |
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