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.
R-40 3870N
Aerojet Rocketdyne – R-40 3870NOverview
| Name | R-40 3870N |
| Manufacturer | Aerojet Rocketdyne |
| Subsystem | Propulsion |
| Classification | Biprop 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 | Biprop Thruster |
| Form Factor | SmallSat |
| Vendor | Aerojet Rocketdyne |
| Heritage | Yes |
| Mass | 10.5 kg |
| Nominal Power | 70.0 W |
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