Development and Characterization of High-Efficiency, High-Specific Impulse Xenon Hall Thrusters

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" Development and Characterization of High-Efficiency, High-Specific Impulse Xenon Hall Thrusters "

Document Type	:	Latin Dissertation
Language of Document	:	English
Record Number	:	149889
Doc. No	:	ET21681
Main Entry	:	Richard Robert Hofer
Title Proper	:	Development and Characterization of High-Efficiency, High-Specific Impulse Xenon Hall Thrusters
Note	:	This document is digital این مدرک بصورت الکترونیکی می باشد
Abstract	:	Most often regarded as a moderate specific impulse (1600 s) space propulsiontechnology, the Hall effect thruster has benefited from considerable theoretical andexperimental research since the 1960's [I-31. Deriving from research on magnetronsand other cross-field plasma sources, the first working devices were reported byAmericans beginning in 1962 [4-10],1 but ultimately the technology was developed inthe former Soviet Union.2 Hall thrusters were first flown in space when the Russiandesign bureau Fakel launched a pair of SPT-60 magnetic layer thrusters with theSoviet Meteor satellite in December 1971 [181. Since that pioneering flight, over onehundred thrusters have flown on Earth orbiting spacecraft, primarily for station..tested for theQ1 PC1 bus cardBoth these projects mere sofixare des elopment efforts tonards contributing to dlfferentaspects of Roboucs and lZ1echatronics projects m the Controls and Roboucs Group..
Subject	:	Electericl tess
	:	برق
electronic file name	:	TL44862.pdf
Title and statement of responsibility and	:	Development and Characterization of High-Efficiency, High-Specific Impulse Xenon Hall Thrusters [Thesis]