A dual-component attitude control thruster injector with a micro-channel liquid collection chamber
An injector and two-component technology, applied in the direction of machines/engines, jet propulsion devices, rocket engine devices, etc., can solve problems such as incomplete isolation of oxygen and fuel channels, interference of propellant atomization quality, explosion, etc., to achieve Excellent mechanical properties, light weight and small volume design, and the effect of improving pulse performance
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[0037] An exemplary embodiment of the present disclosure will be described in more detail below with reference to the accompanying drawings. Although the exemplary embodiments of the present disclosure are shown in the drawings, it is understood that the present disclosure can be implemented in various forms and should not be restricted herein. Instead, it is provided to provide more thoroughly understood the present disclosure, and can communicate the scope of the disclosure to those skilled in the art. It should be noted that the features in the present invention in the present invention can be combined with each other in the case of an unable conflict. The present invention will be described in detail below with reference to the drawings.
[0038] figure 1 It is a schematic structural diagram of a two-component post-liquid lifting thruster that has a tiny flowway set liquid chamber according to an embodiment of the present invention. Such as figure 1As shown, the two-component...
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