Space engine precooling system, working method and spacecraft
The invention provides a space engine pre-cooling system, a working method and a spacecraft. The space engine pre-cooling system comprises a storage tank, an engine, a heat exchange loop heat exchange section and a double-layer transmission pipe. The heat exchange loop heat exchange section is arran...
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Main Authors | , , , , , , |
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Format | Patent |
Language | Chinese English |
Published |
26.05.2023
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Subjects | |
Online Access | Get full text |
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Summary: | The invention provides a space engine pre-cooling system, a working method and a spacecraft. The space engine pre-cooling system comprises a storage tank, an engine, a heat exchange loop heat exchange section and a double-layer transmission pipe. The heat exchange loop heat exchange section is arranged on the peripheral side of the engine; the storage box is communicated with the head of the engine through a double-layer transmission pipe; a loop is arranged between the heat exchange section of the heat exchange loop and the storage box, and the loop flows in a one-way mode, is led out from an interlayer of the double-layer transmission pipe, flows to an engine for heat exchange and then flows back to the storage box; the temperature maintaining device is used for maintaining the temperature of the engine of the space low-temperature propelling system, closed-loop driving is formed through the capillary action and heat exchange steam pressure, and low-temperature propellants are not wasted.
本发明提供了一种空间发动机预冷系统、 |
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Bibliography: | Application Number: CN202211695465 |