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：
Compilation and indexing terms; Copyright 2024 Elsevier Inc;
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
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页码：1 / 12
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