Study of instantaneous regression rate in hybrid rocket motor

被引：0
|
作者：
Yang, Yu-Xin [1 ]
Hu, Chun-Bo [1 ]
Qin, Fei [1 ]
Cai, Ti-Min [1 ]
机构：
[1] National Key Laboratory of Combustion, Flow and Thermo-Structure, Coll. of Astronautics, Northwestern Polytechnical Univ., Xi'an 710072, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2008年 / 29卷 / 05期
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页码：533 / 538
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