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A radiation model for geocentric trajectory calculationsA solar cell degradation model developed for the SECKSPOT trajectory optimization code is presented. The model is based on two analytic expressions, one describing solar cell power degradation as a function of 1 MeV equivalent fluence and cell base resistivity and thickness, and one describing a spatial field of 1 MeV equivalent electron flux. The model extends the latitude range, provides a continuous and smooth representation of the flux field, and provides for changing the cell characteristics. Construction of a 1 MeV electron flux model and of a power loss model are described. It is shown that modeling the 1 MeV flux field as a separate entity allows simple consideration of both front and back shielding, and that the coefficients relating to specific cell damage data can be simply updated using the latest cell damage data once the general analytical characteristics of the model have been established.
Document ID
19750042493
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Malchow, H. L.
Whitney, C. K.
(Charles Stark Draper Laboratory, Inc. Cambridge, Mass., United States)
Date Acquired
August 8, 2013
Publication Date
March 1, 1975
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 75-351
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Electric Propulsion Conference
Location: New Orleans, LA
Start Date: March 19, 1975
End Date: March 21, 1975
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
75A26565
Funding Number(s)
CONTRACT_GRANT: NAS3-18886
Distribution Limits
Public
Copyright
Other

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