Ascent trajectory design method for RBCC-powered vehicle

被引：0
|
作者：
Lu, Xiang [1 ]
He, Guoqiang [1 ]
Liu, Peijin [1 ]
机构：
[1] National Key Laboratory of Combustion, Flow and Thermo-structure, Northwestern Polytechnical University, Xi'an 710072, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2010年 / 31卷 / 07期
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摘要：
19
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页码：1331 / 1337
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