| Propellants Combination Oxidiser/Fuel | Parameter | Value |
| H2O2/ Kerosene | Chamber thrust (vac) | 100 N |
|
| Specific impulse (vac) | 236.48804 s |
|
| Total mass flow rate | 43.12 g/s |
|
| Oxidizer mass flow rate | 37.96 g/s |
|
| Fuel mass flow rate | 5.156 g/s |