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Pioneer Venus Orbiter Electron Temperature ProbeThe Orbiter Electron Temperature Probe (OETP) instrumentation and measurement technique has been designed to perform in-situ measurements of electron temperature and electron and ion density in the ionosphere of Venus. Adaptive sweep voltage circuitry continuously tracks the changing electron temperature and spacecraft potential while auto-ranging electrometers adjust their gain in response to the changing plasma density. Control signals used in the instrument to achieve this automatic tracking provide a continuous monitor of the ionospheric parameters without telemetering each volt-ampere curve. Internal data storage permits high data rate sampling of selected raw characteristic curves for low rate transmission to earth. These curves are used to verify or correct the inflight processed data. Sample in orbit measurements are presented to demonstrate instrument performance.
Document ID
19800046668
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Krehbiel, J. P.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Brace, L. H.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Theis, R. F.
(NASA Goddard Space Flight Center Laboratory for Planetary Atmospheres, Greenbelt, Md., United States)
Cutler, J. R.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Pinkus, W. H.
(Michigan, University Ann Arbor, Mich, United States)
Kaplan, R. B.
(Ultramet, Inc. Pacoima, Calif., United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Publication Information
Publication: IEEE Transactions on Geoscience and Remote Sensing
Volume: GE-18
Subject Category
Spacecraft Instrumentation
Accession Number
80A30838
Distribution Limits
Public
Copyright
Other

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