Art

J-GLOBAL ID：201702221362240551   Reference number：17A0063562

Effect on self-pressurization characteristics and mass loss of thermodynamic vent system for refrigerant R141b by heat load

R141B 熱力学排気システムの自己加圧特性と排気損失に及ぼす熱負荷の影響【JST・京大機械翻訳】

Author (7)： Chen Zhongcan (Institute of Refrigeration and Cryogenics, Shanghai Jiao Tong University) ,  Huang Yonghua (Institute of Refrigeration and Cryogenics, Shanghai Jiao Tong University) ,  Wang Bin (Institute of Refrigeration and Cryogenics, Shanghai Jiao Tong University) ,  Li Peng (Aerospace System Engineering Shanghai) ,  Sun Peijie (Aerospace System Engineering Shanghai) ,  Wang Tianxiang (State Key Laboratory of Technologies in Space Cryogenic Propellants) ,  Cui Jiaxun (Institute of Refrigeration and Cryogenics, Shanghai Jiao Tong University)
Material： Huagong Xuebao  (Kako Gakuho)
Volume： 67  Issue： 10  Page： 4047-4054  Publication year： 2016 
JST Material Number： E0215B  ISSN： 0438-1157  CODEN： HUKHAI  Document type： Article
Article type： 原著論文  Country of issue： China (CHN)  Language： CHINESE (ZH)

Abstract/Point： In order to study the fundamen...

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Thesaurus term： control system (computer) ,  *thermal load ,  gravity ,  storage tank ,  *Thermodynamics ,  pressure loss ,  low temperature ,  direct injection ,  pressure control ,  *exhaust ,  propellant ,  supercharging ,  *pressurization ,  steam separation ,  working fluid ,  *action and behavior

Author keywords (5)： R141b ,  thermodynamics ,  pressure control ,  heat transfer ,  phase change

JST classification (3)： Rocket engines  (PB02050J) ,  Energy storage  (LC02000F) ,  Flying object design and structure  (QK04010H)

Terms in the title (5)： 熱力学 ,  排気 ,  自己 ,  加圧 ,  熱負荷