Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: System Design

被引：0

作者：

Kawasaki, Akira ^{[1
]}

Matsuyama, Koichi ^{[1
]}

Matsuoka, Ken ^{[1
]}

Watanabe, Hiroaki ^{[1
]}

Itouyama, Noboru ^{[1
]}

Goto, Keisuke ^{[1
]}

Ishihara, Kazuki ^{[1
]}

Buyakofu, Valentin ^{[1
]}

Noda, Tomoyuki ^{[1
]}

Kasahara, Jiro ^{[1
]}

Matsuo, Akiko ^{[1
]}

Funaki, Ikkoh ^{[2
]}

Nakata, Daisuke ^{[3
]}

Uchiumi, Masaharu ^{[4
]}

Habu, Hiroto ^{[4
]}

Takeuchi, Shinsuke ^{[3
]}

Arakawa, Satoshi ^{[3
]}

Masuda, Junichi ^{[3
]}

Maehara, Kenzi ^{[3
]}

Nakao, Tatsuro ^{[3
]}

Yamada, Kazuhiko ^{[3
]}

机构：

[1] Nagoya University, Aichi, Nagoya,464-8603, Japan

[2] Keio University, Kanagawa, Yokohama,223-8522, Japan

[3] Japan Aerospace Exploration Agency, Kanagawa, Sagamihara,252-5210, Japan

[4] Muroran Institute of Technology, Hokkai-do, Muroran,050-8585, Japan

来源：

AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 | 2022年

关键词：

D O I：

AIAA 2022-0229

中图分类号：

学科分类号：

摘要：

Detonation - Sounding rockets - Spacecraft propulsion - Propellants - Space research

引用

页码：1 / 12

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