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采用低温制冷机与低温贮箱耦合的方式,可以实现低温推进剂在太空环境下的零蒸发贮存。从系统分析、机理研究及试验研究三个方面对低温推进剂零蒸发贮存技术的现状进行了综述,阐述了现有的系统分析方法、理论分析模型及零蒸发试验方案,可为低温推进剂空间贮存的发展提供参考。
The use of low-temperature refrigerator and low-temperature tank coupling means, you can achieve low-temperature propellant storage in space-zero environment. The current status of cryogenic propellant zero-evaporation storage technology is reviewed from the aspects of system analysis, mechanism research and experimental research. The existing system analysis methods, theoretical analysis models and zero-evaporation test scheme are described, which can be used for cryogenic propellant space Storage development for reference.