Description
The R-40 3870N is a Biprop Thruster developed by Aerojet Rocketdyne. R-40 3870N Biprop Thruster is designed for SmallSat with a mass of 10.5 kg and an average power consumption of 70 W.
The R-40 3870N is a Biprop Thruster developed by Aerojet Rocketdyne. R-40 3870N Biprop Thruster is designed for SmallSat with a mass of 10.5 kg and an average power consumption of 70 W.
Name | R-40 3870N |
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 | 10.5 kg |
Nominal Power | 70.0 W |