Description
Space Solution’s 2500 N bipropellant thruster has a specific impulse of 293 seconds with a chamber pressure of 20 bar. The thruster is designed to use H2O2 90% wt / kerosene.
2500N Bipropellant Engine
Space Solutions – 2500N Bipropellant EngineOverview
| Name | 2500N Bipropellant Engine |
| Manufacturer | Space Solutions |
| Subsystem | Propulsion |
| Classification | Biprop Thruster |
| Form Factor | SmallSat |
Vendor Overview
| Vendor Name | Space Solutions |
| Vendor Website | http://www.spacesolutions.co.kr/ |
| Vendor Location | Korea |
Vendor Request for Information Form
SPECIFICATIONS
| Subsystem | Propulsion |
| Classification | Biprop Thruster |
| Form Factor | SmallSat |
| Vendor | Space Solutions |
| Heritage | N/A |
