Micro liquid fuel propulsion system used in micro-nano satellite
A micro-liquid, micro-nano satellite technology, applied in the field of satellite propulsion systems, to achieve the effects of light weight, low energy consumption and small size
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[0022] see figure 1 As shown, the liquid fuel micro-propulsion system of the present invention mainly includes: a pressurized gas generator 1, a micro-propeller 12, a fuel storage tank 4 providing liquid fuel for the micro-propulsor 12, and the pressurized gas generator 1 is used for fuel storage. The storage tank 4 is inflated and pressurized; the fuel storage tank 4 is divided into a liquid storage part 42 for storing liquid fuel by a diaphragm 5, and a gas storage part 41 communicated with the pressurized gas generator 1 through the gas delivery pipeline 13, in order to reduce The amount of medicine in the pressurized gas generator is filled with carbon dioxide gas in advance in the gas storage part 41 of the fuel storage tank 4. The function of the diaphragm 5 is to separate the liquid fuel from the pressurized gas, so that the liquid can be separated under the state of weightlessness in space. No air bubbles are entrained and discharged smoothly. There are pressure sensor...
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