Hypergolic propellant rocket engine combustion instability studies

被引：0
|
作者：
Nie, Wan-Sheng [1 ]
Zhuang, Feng-Chen [1 ]
机构：
[1] Inst. of Command Technology, Bijing 101416, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2000年 / 21卷 / 04期
关键词：
Hypergolic rocket propellants;
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：63 / 65
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