| Propellants Combination Oxidiser/Fuel | Combustion Pressure (MPa) | Mixture Ratio (R) | Flame Temperature (K) | Isp (S) | Thrust (N) | Total Mass Flow (Oxidizer + Fuel) (g/s) |
| H2O2/Kerosene | 1.277 | 7.35 | 266.7 | 273 | 100 | 37.3516 |