Planetary lander propulsion system passivation device and method
The invention provides a planetary lander propulsion system passivation device and method. The planetary lander propulsion system passivation device comprises a gas cylinder, a gas circuit electric explosion valve, a pressure reducing valve, a passivation electric explosion valve, an oxygen diaphrag...
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creator | LIN SEN HAN QUANDONG PAN YILI BI SHAOKANG YANG XIANZHAO WANG YAPING TAN ZHIYUN |
description | The invention provides a planetary lander propulsion system passivation device and method. The planetary lander propulsion system passivation device comprises a gas cylinder, a gas circuit electric explosion valve, a pressure reducing valve, a passivation electric explosion valve, an oxygen diaphragm type storage tank, a combustion diaphragm type storage tank, a pressure sensor and a passivation engine. The gas cylinder is connected with the passivation engine through a pipeline, and the gas circuit electric explosion valve, the pressure reducing valve, the oxygen diaphragm type storage tank and the combustion diaphragm type storage tank are sequentially arranged on the pipeline; the passivation engine is used for ignition when a propellant is passivated; the oxygen diaphragm type storage tank and the combustion diaphragm type storage tank are arranged in parallel; diaphragms are arranged in the oxygen diaphragm type storage tank and the combustion diaphragm type storage tank and used for separating gas and l |
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The planetary lander propulsion system passivation device comprises a gas cylinder, a gas circuit electric explosion valve, a pressure reducing valve, a passivation electric explosion valve, an oxygen diaphragm type storage tank, a combustion diaphragm type storage tank, a pressure sensor and a passivation engine. 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language | chi ; eng |
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subjects | AIRCRAFT AVIATION COSMONAUTICS PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR |
title | Planetary lander propulsion system passivation device and method |
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