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�������պ����ѧѧ�� 2001, Vol. 27 Issue (5) :615-618    DOI:
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Experiment Data Acquisition System of Low Power Arcjet Thruster
TANG Hai-bin1, JI Luo-shuan2, LIU Yu1, DAI Wu-ye1*
1. Beijing University of Aeronautics and Astronautics, School of Astronautics;
2. LangFang College of Army and Missile, Foundation Department

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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.
Keywords�� arc jet engines   experiment   data acquisition     
Received 2000-02-21;
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������, ����˨, ����, ����Ҷ.С���ʵ绡�������巢����ʵ�����ݲɼ�ϵͳ[J]  �������պ����ѧѧ��, 2001,V27(5): 615-618
TANG Hai-bin, JI Luo-shuan, LIU Yu, DAI Wu-ye.Experiment Data Acquisition System of Low Power Arcjet Thruster[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2001,V27(5): 615-618
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