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 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).
Name | MR-104H 510N |
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 | 2.4 kg |
Nominal Power | 60.1 W |