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A Fully Integrated Micro-Magnometer/Microspacecraft for Multipoint Measurements: The Free-Flyer Magnometer

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dc.contributor.author Goldstein, R. en_US
dc.contributor.author Miller, L. N. en_US
dc.contributor.author Fossum, E. en_US
dc.contributor.author Pain, B. en_US
dc.contributor.author Randolph, J. E. en_US
dc.contributor.author Turner, P. R. en_US
dc.contributor.author Cutting, E. en_US
dc.date.accessioned 2004-09-30T03:30:34Z
dc.date.available 2004-09-30T03:30:34Z
dc.date.issued 1995-04 en_US
dc.identifier.citation Santa Fe, New Mexico, USA en_US
dc.identifier.clearanceno 96-0316 en_US
dc.identifier.uri http://hdl.handle.net/2014/24298
dc.description.abstract In the decades since the advent of in situ plasma measurements on board spacecraft, the instrumentation has grown bigger, heavier, and more complex as our understanding of space plasmas improves and our appetite for more information increases...There has thus been a recent interest in the miniaturization of both spacecraft and the instrument payload... This paper describes the results and status of an ongoing design study to understand the problems and trade space of fully integrating an instrument into a micro-spacecraft. en_US
dc.format.extent 869691 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other plasma plasma measurement space plasma en_US
dc.title A Fully Integrated Micro-Magnometer/Microspacecraft for Multipoint Measurements: The Free-Flyer Magnometer en_US


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