Art
J-GLOBAL ID：200902005559322516   Reference number：91A0432202

Performance of double-stage-discharge hall ion thruster.

二段階の放電を利用したホール型イオン推進機の性能
Author (2)：
YAMAGIWA Y

About YAMAGIWA Y

(Shizuoka Univ., Hamamatsu-shi, JPN)

About Shizuoka Univ., Hamamatsu-shi, JPN

, 
KURIKI K

About KURIKI K

(Inst. Space and Astronautical Science, Sagamihara-shi, JPN)

About Inst. Space and Astronautical Science, Sagamihara-shi, JPN


Material：
Journal of Propulsion and Power  (J Propul Power)

About Journal of Propulsion and Power


Volume： 7  Issue： 1  Page： 65-70  Publication year： Jan. 1991 
JST Material Number： C0207B  ISSN： 1533-3876  CODEN： JPPOEL  Document type： Article
Article type： 原著論文  Country of issue： United States (USA)  Language： ENGLISH (EN)
Thesaurus term：
Thesaurus term/Semi thesaurus term
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All keywords is available on JDreamIII(charged).
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ion engine

About ion engine

,...
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JST classification (1)：
JST classification
Category name(code) classified by JST.
Rocket engines 
(PB02050J)

About Rocket engines

Terms in the title (4)：
Terms in the title
Keywords automatically extracted from the title.
段階

About 段階

, 
放電

About 放電

, 
ホール

About ホール

, 
イオン推進機

About イオン推進機


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