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タイトルOverview of the Development of the Solar Electric Propulsion Technology Demonstration Mission 12.5-kW Hall Thruster
本文(外部サイト)http://hdl.handle.net/2060/20140017335
著者(英)Verhey, Timothy; Haag, Thomas; Polk, James; Myers, James; Mikellides, Ioannis; Chang, Li; Griffith, Christopher; Clayman, Lauren; Kamhawi, Hani; Shastry, Rohit; Yim, John; Thomas, Robert; Hofer, Richard; Williams, George; Herman, Daniel; Huang, Wensheng; Goebel, Dan
著者所属(英)NASA Glenn Research Center
発行日2014-07-28
言語eng
内容記述NASA is developing mission concepts for a solar electric propulsion technology demonstration mission. A number of mission concepts are being evaluated including ambitious missions to near Earth objects. The demonstration of a high-power solar electric propulsion capability is one of the objectives of the candidate missions under consideration. In support of NASAs exploration goals, a number of projects are developing extensible technologies to support NASAs near and long term mission needs. Specifically, the Space Technology Mission Directorate Solar Electric Propulsion Technology Demonstration Mission project is funding the development of a 12.5-kW magnetically shielded Hall thruster system to support future NASA missions. This paper presents the design attributes of the thruster that was collaboratively developed by the NASA Glenn Research Center and the Jet Propulsion Laboratory. The paper provides an overview of the magnetic, plasma, thermal, and structural modeling activities that were carried out in support of the thruster design. The paper also summarizes the results of the functional tests that have been carried out to date. The planned thruster performance, plasma diagnostics (internal and in the plume), thermal, wear, and mechanical tests are outlined.
NASA分類Spacecraft Propulsion and Power
レポートNOGRC-E-DAA-TN16764
権利Copyright, Distribution as joint owner in the copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/61633


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