摘要: |
介绍了低温液体自然循环预冷方案, 并以液氮为模拟推进剂, 进行一系列循环预冷模拟试验, 包括常压或增压环境、气相回流或液相回流、小管径或大管径、回流管绝热或裸露、自流或引射等各种组合。通过分析对比各状态试验时系统所获得的温度、压力数据, 得出气相回流循环预冷试验较液相回流循环预冷试验更能快速、持续地预冷系统, 增压和引射在特定条件下有利于系统保持循环状态等结论。 |
关键词: 低温推进剂火箭发动机 低温冷却 自然循环+ 试验 |
DOI: |
分类号:V434.14 |
基金项目: |
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Simulation test of natural circulation precooling for cryogenic pump system |
LI Qi-fen, CHEN Guo-bang, XIE Xue-mei, ZHONG Yi-kui, ZHENG Xi-liang, BAO Rui
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Inst. of Refrigeration and Cryogenics, Zhejiang Univ., Hangzhou 310027,China
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Abstract: |
A series of experiments were made to investigate cryogenic liquid natural circulation precooling scheme. Liquid nitrogen is used as simulation propellant and experiments including normal pressure or pressurizing environment, gas-phase reflux or liquid-phase reflux, different pipe diameters, bare or insulated reflux pipe, natural or injecting circulation, etc are carried out. By analyzing the experimental results,it is found that the gas-phase reflux circulation is quicker and longer than the liquid-phase inlet reflux circulation in precooling system while pressurization and injection are suggested to keep circulation in some states. |
Key words: Cryogenic propellant rocket engine Cryocooling Natural circulation Test |