Volume 32 Issue 3
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Study on subcooled technology for cryogenic propellants[J]. Journal of Aerospace Power, 2017, 32(3): 762-768. doi: 10.13224/j.cnki.jasp.2017.03.031
Citation: Study on subcooled technology for cryogenic propellants[J]. Journal of Aerospace Power, 2017, 32(3): 762-768. doi: 10.13224/j.cnki.jasp.2017.03.031

Study on subcooled technology for cryogenic propellants

doi: 10.13224/j.cnki.jasp.2017.03.031
  • Received Date: 2015-07-05
  • Publish Date: 2017-03-28
  • Three subcooled methods,including the subcooled technology of heat transfer, pumping down decompression and injecting cooled helium for cryogenic propellants were summarized. By comparing advantages and disadvantages of three methods, the subcooled technology of pumping down decompression was recommended to be used on the entire loading process of ground. Based on thermodynamics theory, expressions of consumption, refrigeration capacity, pumping down time and lowest pumping speed were derived for the subcooled technology of pumping down decompression. The researches showed that consumption of cryogenic propellants was mainly used for its temperature drop, then the proportion for offsetting external leakage heat and special heat of tank material was very small, for instance, the relative consumption of its temperature drop, special heat of tank material, and external leakage heat for liquid hydrogen was 10.94%,0.38%,0.098%, respectively. The arithmetic accurately calculating consumption of cryogenic propellants was recommended to reduce launch costs of launch vehicle and enhance utilization of cryogenic propellants. Compared with the exiting formula, its relative error was 18%.

     

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