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《GRYOGENICS》 1994-01
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Temperature Control of the Low Temperature Propellant

Yang Jinning  
By means of the analysis of the results from lots of ground testsand flight of the third stage of a low temperature propellant launch vehi-cle,this article has concluded sotne factocs to affect the temperature oflow temperature propellant as well as their responsible control methods,and made a scene of the new type of pressurization system and tempera- ture control technology.
【CateGory Index】: V434.13
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