Description
A 225 N monopropellant engine developed by Space Solutions. The thruster the propellant H2O2, has a mass of 0.85 kg, and a specific impulse of 170 seconds.
A 225 N monopropellant engine developed by Space Solutions. The thruster the propellant H2O2, has a mass of 0.85 kg, and a specific impulse of 170 seconds.
Name | 250N Monopropellant Thruster |
Manufacturer | Space Solutions |
Subsystem | Propulsion |
Classification | Monoprop Thruster |
Form Factor | SmallSat |
Vendor Name | Space Solutions |
Vendor Website | http://www.spacesolutions.co.kr/ |
Vendor Location | Korea |
Subsystem | Propulsion |
Classification | Monoprop Thruster |
Form Factor | SmallSat |
Vendor | Space Solutions |
Heritage | N/A |
Mass | 0.85 kg |