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.
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.
Name | 2500N Bipropellant Engine |
Manufacturer | Space Solutions |
Subsystem | Propulsion |
Classification | Biprop Thruster |
Form Factor | SmallSat |
Vendor Name | Space Solutions |
Vendor Website | http://www.spacesolutions.co.kr/ |
Vendor Location | Korea |
Subsystem | Propulsion |
Classification | Biprop Thruster |
Form Factor | SmallSat |
Vendor | Space Solutions |
Heritage | N/A |