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Retarding potential analyzer for the Pioneer-Venus Orbiter MissionThe retarding potential analyzer on the Pioneer-Venus Orbiter Mission has been designed to measure most of the thermal plasma parameters within and near the Venusian ionosphere. Parameters include total ion concentration, concentrations of the more abundant ions, ion temperatures, ion drift velocity, electron temperature, and low-energy (0-50 eV) electron distribution function. To accomplish these measurements on a spinning vehicle with a small telemetry bit rate, several functions, including decision functions not previously used in RPA's, have been developed and incorporated into this instrument. The more significant functions include automatic electrometer ranging with background current compensation; digital, quadratic retarding potential step generation for the ion and low-energy electron scans; a current sampling interval of 2 ms throughout all scans; digital logic inflection point detection and data selection; and automatic ram direction detection. Extensive numerical simulation and plasma chamber tests have been conducted to verify adequacy of the design for the Pioneer Mission.
Document ID
19790050935
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Knudsen, W. C.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Bakke, J.
(Lockheed Research Laboratories Palo Alto, Calif., United States)
Spenner, K.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Novak, V.
(Fraunhofer-Gessellschaft zur Foerderung der angewandten Forschung Freiburg im Breisgau, Germany)
Date Acquired
August 9, 2013
Publication Date
April 1, 1979
Publication Information
Publication: Space Science Instrumentation
Volume: 4
Subject Category
Spacecraft Instrumentation
Accession Number
79A34948
Funding Number(s)
CONTRACT_GRANT: BMFT-01-DO238(RV 14-B 28/73)
CONTRACT_GRANT: NAS2-8811
Distribution Limits
Public
Copyright
Other

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