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Volume 27 Issue 5
May  2001
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Journal of Beijing University of Aeronautics and Astronautics  > 2001  >  27(5): 615-618.
TANG Hai-bin, JI Luo-shuan, LIU Yu, et al. Experiment Data Acquisition System of Low Power Arcjet Thruster[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(5): 615-618. (in Chinese)
Citation: TANG Hai-bin, JI Luo-shuan, LIU Yu, et al. Experiment Data Acquisition System of Low Power Arcjet Thruster[J]. Journal of Beijing University of Aeronautics and Astronautics, 2001, 27(5): 615-618. (in Chinese)
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Experiment Data Acquisition System of Low Power Arcjet Thruster

  • 1.

    Beijing University of Aeronautics and Astronautics, School of Astronautics

  • 2. LangFang College of Army and Missile, Foundation Department

  • Received Date: 21 Feb 2000
  • Publish Date: 31 May 2001
    Abstract
  • With an introduction to the experimental setting and the data acquisition system of low power Arcjet thruster, measuring principles of engine operating thrust, current and voltage were highlighted, together with descriptions about measuring methods of parameters, hardware configuration, and performance of data acquisition system, as wellas rules and methods of software development. Typical experimental results were given to reflect the experiment process exactly.

     

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  • [1] 汤海滨,祝寿恩,刘 宇.10 kW固体推进剂燃烧驱动CO2气动激光数据采集系统[J].强激光与粒子束,1999,11(2):159~164． [2] 沈兰荪.数据采集技术[M]．北京:中国科技大学出版社,1990． [3] 吕振中,夏青松.微型计算机数据采集与处理的小型系统[J].推进技术,1994,1:73~77．
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