| Propellants Combination Oxidiser/Fuel | Parameter | Value |
| H2O2/Kerosene | Chamber thrust (vac) | 97.97 N |
|
| Specific impulse (vac) | 235.91868 s |
|
| Total mass flow rate | 42.34 g/s |
|
| Oxidizer mass flow rate | 37.27 g/s |
|
| Fuel mass flow rate | 5.07 g/s |