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机构地区:[1]College of Aerospace Science and Engineering,Nati onal University of Defense Technology
出 处:《Journal of Measurement Science and Instrumentation》2013年第2期103-110,共8页测试科学与仪器(英文版)
基 金:National Natural Science Foundation of China (No.91216201, No.51205403)
摘 要:The applications of the micro-thrust e r and the challenges of micro-thrust measuring are introduced.The developments in measuring techniques for the micro-thrust are reviewed.Micro-thrust measu rements have previously been made either directly by mounting thrusters to the m easurement system or indirectly by mounting a target in the direct path of the e jected propellant.Several typical direct and indirect thrust-stands are presen ted and discussed in detail to illustrate the principles.Typical calibration me thods are also expounded.Finally,the resolution,uncertainty and thrust range of each thrust-stand are given,which may be helpful for the future thrust stan d design and micro-thrusters research.
关 键 词:MICRO-THRUSTER thrust stand thrust measurement CALIBRATION direct measurement indirect measurement
分 类 号:V439[航空宇航科学与技术—航空宇航推进理论与工程]
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