文献
J-GLOBAL ID:201802239627758463
整理番号:18A2046040
ホロー陰極を用いた印加磁場MPDスラスタの動作特性
Operation Characteristics of Applied-Field Magnetoplasmadynamics Thruster Using Hollow Cathode
著者 (9件):
KASUGA Hayato
(Department of Aerospace Engineering, Nagoya University)
,
JEONG Jeohun
(Department of Aerospace Engineering, Nagoya University)
,
MIZUTANI Keisuke
(Department of Aerospace Engineering, Nagoya University)
,
IWAKAWA Akira
(Department of Aerospace Engineering, Nagoya University)
,
SASOH Akihiro
(Department of Aerospace Engineering, Nagoya University)
,
KOJIMA Kohei
(Mitsubishi Heavy Industries, Ltd)
,
KIMURA Tatsuya
(Mitsubishi Heavy Industries, Ltd)
,
KAWAMATA Yoshihiro
(Mitsubishi Heavy Industries, Ltd)
,
YASUI Masaaki
(Mitsubishi Heavy Industries, Ltd)
資料名:
Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan (Web)
(Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan (Web))
巻:
16
号:
1
ページ:
69-74(J-STAGE)
発行年:
2018年
JST資料番号:
U0121A
ISSN:
1884-0485
資料種別:
逐次刊行物 (A)
記事区分:
原著論文
発行国:
日本 (JPN)
言語:
英語 (EN)