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小功率电弧等离子体发动机实验数据采集系统

Experiment Data Acquisition System of Low Power Arcjet Thruster

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【作者】 汤海滨姬罗栓刘宇戴梧叶

【Author】 TANG Hai bin (Beijing University of Aeronautics and Astronautics, School of Astronautics) JI Luo shuan (LangFang College of Army and Missile, Foundation Department) LIU Yu DAI Wu ye (Beijing University of Aeronautics and Astronautics, School of A

【机构】 北京航空航天大学宇航学院廊坊陆军导弹学院基础部北京航空航天大学宇航学院

【摘要】 介绍了小功率电弧等离子体发动机的实验装置及数据采集系统 ,阐述其结构组成及工作过程 ,重点介绍了发动机工作推力、电流和电压的测量原理 ,并对数据采集系统的硬件配置、性能及软件的编制的原则、方法作了主要说明 ,给出典型实验所测结果 .测量结果准确反映了实验工作过程 .

【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 well as rules and methods of software development. Typical experimental results were given to reflect the experiment process exactly.

【关键词】 电弧喷气发动机实验数据采集
【Key words】 arc jet enginesexperimentdata acquisition
  • 【文献出处】 北京航空航天大学学报 ,Journal of Beijing University of Aeronautics and Astronautics , 编辑部邮箱 ,2001年05期
  • 【分类号】V439.2
  • 【被引频次】4
  • 【下载频次】134
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