Zobrazeno 1 - 10 of 84 pro vyhledávání: '"Hiroto HABU"'
1
Akademický článek
Study on peristaltic continuous mixing conveyor for composite propellant slurry mixing
Autor: Yasuyuki YAMADA, Shun YOSHIHAMA, Akihiro IWASAKI, Kyota ASHIGAKI, Kotaro MATUMOTO, Hiroto HABU, Taro NAKAMURA
Publikováno v: Nihon Kikai Gakkai ronbunshu, Vol 83, Iss 850, Pp 16-00576-16-00576 (2017)
In recent years, the demand for rocket launching has increased due to the development of space technology. However, using inexpensive rockets is not always possible. Although the cost of solid-propellant rockets is relatively reasonable, safely manuf
Externí odkaz: https://doaj.org/article/e479309a64da4162ae4e23cb42b5c043
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2
Conceptual Design of Small-Sized Thruster Using Laser Ignition of High-Energy Monopropellant
Autor: Noboru Itouyama, Asato Wada, Hiroto Habu, Yoshimichi Sago
Publikováno v: Journal of Propulsion and Power. 39:416-425
Ammonium dinitramide (ADN)-based energetic ionic liquid propellants (ADN-EILPs) present considerable potential as monopropellants due to high energy density, high thermal/chemical stability, and low toxicity. Consequently, a chemical thruster system
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::9d60678455d1fa8885c4e328b37fbca1
https://doi.org/10.2514/1.b38880
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3
Space Flight Demonstration of Rotating Detonation Engine Using Sounding Rocket S-520-31
Autor: Keisuke Goto, Ken Matsuoka, Koichi Matsuyama, Akira Kawasaki, Hiroaki Watanabe, Noboru Itouyama, Kazuki Ishihara, Valentin Buyakofu, Tomoyuki Noda, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Masaharu Uchiumi, Hiroto Habu, Shinsuke Takeuchi, Satoshi Arakawa, Junichi Masuda, Kenji Maehara, Tatsuro Nakao, Kazuhiko Yamada
Publikováno v: Journal of Spacecraft and Rockets. 60:273-285
To create a new flyable detonation propulsion system, a detonation engine system (DES) that can be stowed in sounding rocket S-520-31 has been developed. This paper focused on the first flight demonstration in the space environment of a DES-integrate
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::aaf525ad2eda24688794d2af7015e1cf
https://doi.org/10.2514/1.a35401
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4
Flight Demonstration of Pulse Detonation Engine Using Sounding Rocket S-520-31 in Space
Autor: Valentin Buyakofu, Ken Matsuoka, Koichi Matsuyama, Akira Kawasaki, Hiroaki Watanabe, Noboru Itouyama, Keisuke Goto, Kazuki Ishihara, Tomoyuki Noda, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Masaharu Uchiumi, Hiroto Habu, Shinsuke Takeuchi, Satoshi Arakawa, Junichi Masuda, Kenji Maehara, Tatsuro Nakao, Kazuhiko Yamada
Publikováno v: Journal of Spacecraft and Rockets. 60:181-189
A detonation engine system is successfully demonstrated for the first time in space using sounding rocket S-520-31 of the Japan Aerospace Exploration Agency/Institute of Space Astronautical Science. Detailed flight results of an S-shaped pulse detona
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::922a3ef21999266da51e354450c00177
https://doi.org/10.2514/1.a35394
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5
Akademický článek
Viscosity of Aluminum/Hydroxyl-terminated polybutadiene suspensions using bimodal Aluminum particles.
Autor: Kotaro Matsumoto1 matsumoto.koutarou@nihon-u.ac.jp, Hiroto Habu2
Publikováno v: Science & Technology of Energetic Materials. 2022, Vol. 83 Issue 2, p8-13. 6p.
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