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タイトルIon beam plume and efflux characterization flight experiment study
本文(外部サイト)http://hdl.handle.net/2060/19780004197
著者(英)Sellen, J. M., Jr.; Rosiak, G.; Komatsu, G. K.; Cole, A.; Zafran, S.
著者所属(英)TRW Defense and Space Systems Group
発行日1977-12-01
言語eng
内容記述A flight experiment and flight experiment package for a shuttle-borne flight test of an 8-cm mercury ion thruster was designed to obtain charged particle and neutral particle material transport data that cannot be obtained in conventional ground based laboratory testing facilities. By the use of both ground and space testing of ion thrusters, the flight worthiness of these ion thrusters, for other spacecraft applications, may be demonstrated. The flight experiment definition for the ion thruster initially defined a broadly ranging series of flight experiments and flight test sensors. From this larger test series and sensor list, an initial flight test configuration was selected with measurements in charged particle material transport, condensible neutral material transport, thruster internal erosion, ion beam neutralization, and ion thrust beam/space plasma electrical equilibration. These measurement areas may all be examined for a seven day shuttle sortie mission and for available test time in the 50 - 100 hour period.
NASA分類SPACECRAFT PROPULSION AND POWER
レポートNO78N12140
NASA-CR-135275
権利No Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/180573


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