Description
MR-104H 510N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 2.40 kg (includes engine and valves), with a specific impulse of 223 to 237 sec and a thrust of 201.0 to 554.2 N (steady state).
MR-104H 510N
Aerojet Rocketdyne – MR-104H 510NOverview
| Name | MR-104H 510N |
| 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 |
Vendor Request for Information Form
SPECIFICATIONS
| Subsystem | Propulsion |
| Classification | Monoprop Thruster |
| Form Factor | SmallSat |
| Vendor | Aerojet Rocketdyne |
| Heritage | Yes |
| Mass | 2.4 kg |
| Nominal Power | 60.1 W |
