Conceptual Design Optimization of Several Types of Fully Reusable Winged Launch Vehicles
Conceptual Design Optimization of Several Types of Fully Reusable Winged Launch Vehicles
复制标题
几种完全可重复使用有翼运载火箭概念设计优化
DOI：
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发表时间：
2017
期刊：
影响因子：
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通讯作者：
Takahiro Fujikawa and Koichi Yonemoto
中科院分区：
文献类型：
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作者：
高橋聖幸;明官学;Francesca Gnani;Henny Bottini;岩川輝;大西直文;佐宗章弘;Masayuki Takahashi and Naofumi Ohnishi;藤川貴弘，照井勇輔，渡邉真也，米本浩一;Koichi Yonemoto and Takahiro Fujikawa;一ノ宮浩祐，藤川貴弘，米本浩一;Takahiro Fujikawa and Koichi Yonemoto
