| 摘要 |
PROBLEM TO BE SOLVED: To provide a method and a device for feeding a combination of hydrocarbon and oxidizing agent propulsion fuel to a rocket engine for eliminating the problem of instability in a large chamber. SOLUTION: The method and the device are disclosed for feeding the combination of the propulsion fuel to the rocket engine. This method includes a step of supplying a flow of hydrocarbon propulsion fuel, a step of increasing pressure of the hydrocarbon propulsion fuel, a step of decomposing the hydrocarbon propulsion fuel in a decomposer, a step of introducing the decomposed hydrocarbon propulsion fuel into a combustion chamber of the rocket engine, and a step of introducing an oxidizing agent into the combustion chamber. The device is also disclosed for performing this method. COPYRIGHT: (C)2007,JPO&INPIT |
