Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Takashi Mugitani"'
Autor:
Yoshihisa Aoki, Toshio Fukui, Takehiro Kumagai, Hiroki Takayanagi, Taro Tsukamoto, Takashi Ozawa, Koji Ohga, Satoshi Nomura, Hirofumi Shirouzu, Naomi Takizawa, Shinji Ishimoto, Takashi Mugitani, Hiroka Inoue, Toshiyuki Suzuki, Kazuhisa Fujita, Yoshinori Minami, Toshiaki Daibo, Hirokazu Adachi
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN. 16:19-27
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
Accepted: 2017-09-05
資料番号: PA1810044000
Physical characteristics: Original contains color illustrations
Accepted: 2017-09-05
資料番号: PA1810044000
Autor:
Koichi Yonemoto, Hiroshi Yamasaki, Masatomo Ichige, Yusuke Ura, Guna S. Gossamsetti, Takumi Ohki, Kento Shirakata, Ahsan R. Choudhuri, Shinji Ishimoto, Takashi Mugitani, Hiroya Asakawa, Hideaki Nanri
This paper presents the strategic development plan of winged rockets WIRES (WInged REusable Sounding rocket) aiming at unmanned suborbital winged rocket for demonstrating future fully reusable space transportation technologies, such as aerodynamics,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ec287b12cb6ee7de1269b90317d36549
Publikováno v:
IFAC Proceedings Volumes. 34:229-234
National Space Development Agency of Japan (NASDA) is developing a GPS receiver for H-IIA rocket. The purpose of the use of GPS for H-IIA rocket is to measure its position and velocity on the trajectory. Navigation solutions of GPS are used for the p
Autor:
Toshiyuki SUZUKI, Hiroki TAKAYANAGI, Takashi OZAWA, Satoshi NOMURA, Hiroka INOUE, Naomi TAKIZAWA, Kazuhisa FUJITA, Yoshinori MINAMI, Hirokazu ADACHI, Yoshihisa AOKI, Toshio FUKUI, Toshiaki DAIBO, Takashi MUGITANI, Taro TSUKAMOTO, Shinji ISHIMOTO, Takehiro KUMAGAI, Hirofumi SHIROUZU, Koji OHGA
Publikováno v:
Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan; 2018, Vol. 16 Issue 1, p19-27, 9p
Publikováno v:
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference.
A fully-reusable, two-stage system composed of a winged booster vehicle and a winged orbiter vehicle has been studied as a far-term goal in JAXA. The objective of this study is to clarify technology goals. Research activities to develop key technolog
Autor:
Shinji Ishimoto, Takashi Mugitani, Koichi Yonemoto, Shinichi Sagara, Yoshimasa Ochi, Harunori Nagata, Takaaki Matsumoto
Publikováno v:
The Proceedings of Mechanical Engineering Congress, Japan. 2013:S192022-1