4.7 Article

Progress in research on composite cryogenic propellant tank for large aerospace vehicles

出版社

ELSEVIER SCI LTD
DOI: 10.1016/j.compositesa.2021.106297

关键词

Composite cryogenic propellant tank; Liquid oxygen compatibility; Cryogenic mechanical properties; Anti-leakage

资金

  1. National Key Research and Development of China [2018YFA0702804]
  2. Beijing Institute of Technology Research Fund Program for Young Scholars, National Science and Technology Major Project [2017-V I-0020-0093]
  3. National Natural Science Foundation of China [11602125]

向作者/读者索取更多资源

Prototype linerless composite cryogenic propellant tanks are a trend in developing lightweight space vehicles, offering weight reductions up to 20%-40% and promoting the research of new generations of spacecraft. Progress in research on these tanks by various space agencies is systematically analyzed, with solutions to key technical issues being discussed. The development directions of composite cryogenic propellant tanks are explored for the future.
Compared with traditional metal tanks, prototype linerless composite cryogenic propellant tanks can achieve weight reductions up to 20%-40%. This prototype has recently become the trend in developing lightweight space vehicles. Moreover, this prototype promotes the research and development of new generations of inexpensive, high-capacity and recoverable space vehicles. In this review, the progress in research on composite cryogenic storage tanks by various space agencies is systematically analysed. Several key issues, including liquid oxygen compatibility and cryogenic mechanical and antileakage properties, in the process of manufacturing composite cryogenic tanks are summarised. Various solutions to these technical difficulties are briefly discussed. Finally, the directions that the development of composite cryogenic propellant tanks may take are explored.

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