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.
250N Monopropellant Thruster
Space Solutions – 250N Monopropellant ThrusterOverview
| Name | 250N Monopropellant Thruster |
| Manufacturer | Space Solutions |
| Subsystem | Propulsion |
| Classification | Monoprop Thruster |
| Form Factor | SmallSat |
Vendor Overview
| Vendor Name | Space Solutions |
| Vendor Website | http://www.spacesolutions.co.kr/ |
| Vendor Location | Korea |
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SPECIFICATIONS
| Subsystem | Propulsion |
| Classification | Monoprop Thruster |
| Form Factor | SmallSat |
| Vendor | Space Solutions |
| Heritage | N/A |
| Mass | 0.85 kg |
