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Modeling of environmentally induced transients within satellitesA technique is described that allows an estimation of possible spacecraft charging hazards. This technique, called SCREENS (spacecraft response to environments of space), utilizes the NASA charging analyzer program (NASCAP) to estimate the electrical stress locations and the charge stored in the dielectric coatings due to spacecraft encounter with a geomagnetic substorm environment. This information can then be used to determine the response of the spacecraft electrical system to a surface discharge by means of lumped element models. The coupling into the electronics is assumed to be due to magnetic linkage from the transient currents flowing as a result of the discharge transient. The behavior of a spinning spacecraft encountering a severe substorm is predicted using this technique. It is found that systems are potentially vulnerable to upset if transient signals enter through the ground lines.
Document ID
19870054337
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Stevens, N. John
(Hughes Aircraft Co. Los Angeles, CA, United States)
Barbay, Gordon J.
(Hughes Aircraft Co. Los Angeles, CA, United States)
Jones, Michael R.
(Hughes Aircraft Co. Los Angeles, CA, United States)
Viswanathan, R.
(Hughes Aircraft Co. Los Angeles, CA, United States)
Date Acquired
August 13, 2013
Publication Date
June 1, 1987
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 24
ISSN: 0022-4650
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 85-0387
Accession Number
87A41611
Funding Number(s)
CONTRACT_GRANT: NAS3-23869
Distribution Limits
Public
Copyright
Other

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