Application of high fidelity simulation to LE-X engine development

被引：0

作者：

Watanabe, Daiki ^{[1
,4
]}

Imai, Kazuhiro ^{[1
]}

Ogawara, Akira ^{[1
]}

Yamanishi, Nobuhiro ^{[2
]}

Neghishi, Hideyo ^{[2
]}

Kawatsu, Kaname ^{[2
]}

Kurosu, Akihide ^{[3
]}

Noda, Keiichiro ^{[3
]}

机构：

[1] Mitsubishi Heavy Industries, Ltd.(MHI), Japan

[2] Japan Aerospace Exploration Agency(JAXA), JAXA's Engineering Digital Innovation Center, 2-1-1,Sengen, Tsukuba, Ibaraki, 305-8505, Japan

[3] Japan Aerospace Exploration Agency, Space Transportation Mission Directorate, Japan

[4] Liquid Rocket Engine Design Section, Mitsubishi Heavy Industries, Ltd, 1200, Higashi tanaka, komaki, aichi, 485-8561, Japan

来源：

47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011 | 2011年

关键词：

Compendex;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

Rockets

引用