Research Article
Dynamic Characteristics of LOX/Kerosene Variable Thrust Liquid Rocket Engine Test System Based on General Modular Simulation Method
Table 4
Parameters of the main pipelines.
| | Parameters | LOX | Kerosene | Coolant |
| | Pump inlet (mm) | 76.1 | 76.1 | 42.4 | | Pump outlet (mm) | 42.4 | 42.4 | 42.4 | | Propellant return (mm) | 50 | 42.4 | 42.4 | | Exhaust pipeline (mm) | 25 | / | / | | Overflow pipeline (mm) | 20 | 20 | / |
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