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The Thermal Ion Dynamics Experiment and Plasma Source InstrumentThe Thermal Ion Dynamics Experiment (TIDE) and the Plasma Source Instrument (PSI) have been developed in response to the requirements of the ISTP Program for three-dimensional (3D) plasma composition measurements capable of tracking the circulation of low-energy (0-500 eV) plasma through the polar magnetosphere. This plasma is composed of penetrating magnetosheath and escaping ionospheric components. It is in part lost to the downstream solar wind and in part recirculated within the magnetosphere, participating in the formation of the diamagnetic hot plasma sheet and ring current plasma populations. Significant obstacles which have previously made this task impossible include the low density and energy of the outflowing ionospheric plasma plume and the positive spacecraft floating potentials which exclude the lowest-energy plasma from detection on ordinary spacecraft. Based on a unique combination of focusing electrostatic ion optics and time of flight detection and mass analysis, TIDE provides the sensitivity (seven apertures of about 1 cm squared effective area each) and angular resolution (6 x 18 degrees) required for this purpose. PSI produces a low energy plasma locally at the POLAR spacecraft that provides the ion current required to balance the photoelectron current, along with a low temperature electron population, regulating the spacecraft potential slightly positive relative to the space plasma. TIDE/PSI will: (a) measure the density and flow fields of the solar and terrestrial plasmas within the high polar cap and magnetospheric lobes; (b) quantify the extent to which ionospheric and solar ions are recirculated within the distant magnetotail neutral sheet or lost to the distant tail and solar wind; (c) investigate the mass-dependent degree energization of these plasmas by measuring their thermodynamic properties; (d) investigate the relative roles of ionosphere and solar wind as sources of plasma to the plasma sheet and ring current.
Document ID
19970005117
Acquisition Source
Marshall Space Flight Center
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Moore, T. E.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Chappell, C. R.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Chandler, M. O.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Fields, S. A.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Pollock, C. J.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Reasoner, D. L.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Young, D. T.
(Southwest Research Inst. San Antonio, TX United States)
Burch, J. L.
(Southwest Research Inst. San Antonio, TX United States)
Eaker, N.
(Southwest Research Inst. San Antonio, TX United States)
Waite, J. H., Jr.
(Southwest Research Inst. San Antonio, TX United States)
McComas, D. J.
(Los Alamos National Lab. NM United States)
Nordholdt, J. E.
(Los Alamos National Lab. NM United States)
Thomsen, M. F.
(Los Alamos National Lab. NM United States)
Berthelier, J. J.
(Centre de Recherches en Physique de l'Environnement Saint Maur des Fosses, France)
Robson, R.
(Hughes Aircraft Co. Malibu, CA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Publication Information
Publication: Space Science Reviews
Publisher: Kluwer Academic Publisher
Volume: 71
Subject Category
Plasma Physics
Report/Patent Number
NASA-CR-202622
NAS 1.26:202622
Report Number: NASA-CR-202622
Report Number: NAS 1.26:202622
Accession Number
97N13085
Funding Number(s)
CONTRACT_GRANT: NAS8-38189
CONTRACT_GRANT: NAG8-694
CONTRACT_GRANT: NAG8-114
PROJECT: SwRI Proj. 15-9455
Distribution Limits
Public
Copyright
Public Use Permitted.
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