Micro-impulse measurement of MEMS solid propellant thruster array

被引：0
|
作者：
Li, Chuang-Xin [1 ,2 ]
Yu, Xie-Zheng [1 ,3 ]
Ye, Ying-Hua [1 ]
Shen, Rui-Qi [1 ]
Wang, Cheng-Ling [1 ]
Zhu, Ying [1 ]
机构：
[1] School of Chemical Engineering, Nanjing University of Science and Technology, Nanjing 210094, China
[2] Wuhan Ordnance N. C. O Academy of PLA, Wuhan 430075, China
[3] The 31st Research Institute of CASIC, Beijing 100074, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2013年 / 34卷 / 04期
关键词：
Ballistic pendulum - Impulse - Micro electro mechanical system - Micro thruster - Micro-impulse measurement - Moment of inertia - Propulsion performance - Solid-propellant thrusters;
D O I：
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中图分类号：
学科分类号：
摘要：
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页码：572 / 576
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