SWE,a comprehensive plasma instrument for the WIND spacecraft |
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Authors: | K. W. Ogilvie D. J. Chornay R. J. Fritzenreiter F. Hunsaker J. Keller J. Lobell G. Miller J. D. Scudder E. C. Sittler Jr. R. B. Torbert D. Bodet G. Needell A. J. Lazarus J. T. Steinberg J. H. Tappan A. Mavretic E. Gergin |
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Affiliation: | (1) Interplanetary Physics Branch, Goddard Space Flight Center, 20771 Greenbelt, MA, USA;(2) Physics Department and Space Science Center, Institute for Study of Earth, Oceans, and Space, University of New Hampshire, 03284 Durham, NH, USA;(3) Center for Space Research, Massachusetts Institute of Technology, 02139 Cambridge, MA, USA;(4) Microelectronics Research Laboratory, Boston University, 02215 Boston, MA, USA |
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Abstract: | The Solar Wind Experiment (SWE) on the WIND spacecraft is a comprehensive, integrated set of sensors which is designed to investigate outstanding problems in solar wind physics. It consists of two Faraday cup (FC) sensors; a vector electron and ion spectrometer (VEIS); a strahl sensor, which is especially configured to study the electron strahl close to the magnetic field direction; and an on-board calibration system. The energy/charge range of the Faraday cups is 150 V to 8 kV, and that of the VEIS is 7 V to 24.8 kV. The time resolution depends on the operational mode used, but can be of the order of a few seconds for 3-D measurements. Key parameters which broadly characterize the solar wind positive ion velocity distribution function will be made available rapidly from the GGS Central Data Handling Facility. |
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