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NASCAP/LEO Simulations of Shuttle Orbiter Charging During the SAMPIE ExperimentThe electrostatic charging of the Space Shuttle Orbiter during the operation of the Solar Array Module Plasma Interaction Experiment (SAMPIE) was modeled using the NASA Charging Analyzer Program/ low Earth orbit (NASCAP/LEO) computer code. The SAMPIE experiment consists of an array of various solar cells representing the present technologies. The objectives of the experiment are to investigate the arcing and current collection characteristics of these cells when biased to high potentials in a LEO plasma. NASCAP/LEO (NASA Charging Analyzer Program/Low Earth Orbit) is a is a 3-D code designed to simulate the electrostatic charging of a spacecraft exposed to a plasma at LEO or ground test conditions. At its most extreme configuration, with the largest array segment of the SAMPIE experiment biased + 600 V with respect to the orbiter and facing the ram direction, the computer simulations predict that the orbiter's potential will be approximately -20 V with respect to the plasma.
Document ID
19920013118
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Ricaurte Chock
(Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1992
Publication Information
Publication: 5th Annual Workshop on Space Operations Applications and Research (SOAR 1991)
Publisher: National Aeronautics and Space Administration
Volume: 2
Subject Category
Spacecraft Design, Testing and Performance
Report/Patent Number
NASA/CP-3127/Vol II
Meeting Information
Meeting: Space Operation, Application and Research Symposium
Location: Houston, TX
Country: US
Start Date: July 9, 1991
End Date: July 11, 1991
Sponsors: National Aeronautics and Space Administration, U.S. Air Force Phillips Laboratory, University of Houston - Clear Lake
Accession Number
92N22361
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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