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NASA battery testbed: A designed experiment for the optimization of LEO battery operational parametersSimulation of spacecraft battery operation is implemented. Robust design experiment to obtain optimum battery operational parameters is performed. It is found that short term tests using robust design of experiments can provide guidelines for optimum battery operation. It is decided to use robust design approach to provide guidelines for battery operation on current spacecraft in orbit as batteries age (GRO, UARS, EUVE, TOPEX).
Document ID
19960020595
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Deligiannis, F. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Perrone, D. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
DiStefano, S. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Date Acquired
August 17, 2013
Publication Date
February 1, 1996
Publication Information
Publication: The 1995 NASA Aerospace Battery Workshop
Subject Category
Energy Production And Conversion
Accession Number
96N24144
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19960020567Collected WorksThe 1995 NASA Aerospace Battery Workshop
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