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Prediction Model for the Life of Nickel-cadmium Batteries in Geosynchronous Orbit SatellitesA mathematical model is described which predicts the service life of nickel-cadmium batteries designed for geosynchronous orbit satellites. Regression analysis technique is used to analyze orbital data on second generation trickle charged batteries. The model gives average cell voltage as a function of design parameters, operating parameters and time. The voltage model has the properties of providing a good fit to the data, good predictive capability, and agreement with known battery performance characteristics. Average cell voltage can be predicted to within 0.02 volts for up to 8 years. This modeling shows that these batteries will operate reliably for 10 years. Third-generation batteries are expected to operate even longer.
Document ID
19840025615
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Engleman, J. H.
(Hughes Aircraft Co. Los Angeles, CA, United States)
Zirkes-Falco, M. B.
(Hughes Aircraft Co. Los Angeles, CA, United States)
Bogner, R. S.
(Hughes Aircraft Co. Los Angeles, CA, United States)
Pickett, D. F., Jr.
(Hughes Aircraft Co. Los Angeles, CA, United States)
Date Acquired
August 12, 2013
Publication Date
September 1, 1984
Publication Information
Publication: NASA. Goddard Space Flight Center The 1983 Goddard Space Flight Center Battery Workshop
Subject Category
Electronics And Electrical Engineering
Accession Number
84N33686
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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