| Propellants Combination Oxidiser/Fuel | Parameter (s) | Calculated Results | Simulated Results (RPA) |
| H2O2/Kerosene | Thrust (N) | 100 (Expected) | 97.62 |
|
| Specific Impulse (S) | 273 (Assumed) | 230 |
|
| Total Mass Flow Rate (g/s) | 37. 35 | 43.12 |