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Design and improvement for interstage crossover of the multistage liquid hydrogen pump

  • Jia Wen Li*
  • , Sen Yuan Zhu
  • , Zhong Xiang Liu
  • *此作品的通讯作者
  • Beijing Aerospace Propulsion Institute

科研成果: 期刊稿件文章同行评审

摘要

The results, which obtained by using radial diffuser, show that due to the high loss through the diffuser, the efficiency of the liquid hydrogen pump is lower. The author proposed a design method for continuous channel diffuser of liquid hydrogen pump, and designed a interstage crossover for a liquid hydrogen pump. The testing results indicate that, the loss through the interstage crossover is reduced and the efficiency of the pump is improved.

源语言英语
页(从-至)1072-1075
页数4
期刊Yuhang Xuebao/Journal of Astronautics
27
5
出版状态已出版 - 9月 2006

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