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Comparison of the trapped electron models AE-4 and AE-5 with AE-2 and AE-3Models of geomagnetically trapped electrons are compared to estimate mission flux changes. The differences in the model environments were caused by a change in both the existing environment and the available data from which the models were derived. Different data analysis techniques have also influenced the models. This report compares the dependence of the flux to each of the relevant variables. To show the effects of the model differences, included are a comparison of orbital flux integrations for a range of orbits.
Document ID
19740027144
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hilberg, R. H.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Teague, M. J.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Vette, J. I.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
King, M. L.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1974
Subject Category
Space Sciences
Report/Patent Number
NASA-TM-X-72532
NSSDC-74-13
Report Number: NASA-TM-X-72532
Report Number: NSSDC-74-13
Accession Number
74N35257
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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