Description
The R-42DM 890N is a Biprop Thruster developed by Aerojet Rocketdyne. R-42DM 890N Biprop Thruster is designed for SmallSat with a mass of 7.3 kg and an average power consumption of 45 W.
The R-42DM 890N is a Biprop Thruster developed by Aerojet Rocketdyne. R-42DM 890N Biprop Thruster is designed for SmallSat with a mass of 7.3 kg and an average power consumption of 45 W.
Name | R-42DM 890N |
Manufacturer | Aerojet Rocketdyne |
Subsystem | Propulsion |
Classification | Biprop 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 | Biprop Thruster |
Form Factor | SmallSat |
Vendor | Aerojet Rocketdyne |
Heritage | Yes |
Mass | 7.3 kg |
Nominal Power | 45.0 W |