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  • 1
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    The 2000 NASA Aerospace Battery Workshop (2001)
    In:  CASI
    Details
    Publication Date: 2019-08-17
    Description: This document contains the proceedings of the 33nd annual NASA Aerospace Battery Workshop, hosted by the Marshall Space Flight Center on November 14-16, 2000. The workshop was attended by scientists and engineers from various agencies of the U.S. Government, aerospace contractors, and battery manufacturers, as well as international participation in like kind from a number of countries around the world. The subjects covered included nickel-hydrogen, lithium-ion, lithium-sulfur, and silver-zinc technologies.
    Keywords: Energy Production and Conversion
    Type: NASA/CP-2001-210883 , M-1009 , NAS 1.55:210883 , The 2000 NASA Aerospace Battery Workshop; NASA/CP-2001-210883|The 2000 NASA Aerospace Battery Workshop; Nov 14, 2000 - Nov 16, 2000; Huntsville, AL; United States
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 2
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    The 1999 NASA Aerospace Battery Workshop (2000)
    In:  CASI
    Details
    Publication Date: 2019-08-13
    Description: This document contains the proceedings of the 32nd annual NASA Aerospace Battery Workshop, hosted by the Marshall Space Flight Center on November 16-18, 1999. The workshop was attended by scientists and engineers from various agencies of the US Government, aerospace contractors, and battery manufacturers, as well as international participation in like kind from a number of countries around the world. The subjects covered included nickel-hydrogen, nickel-cadmium, lithium-ion, and silver-zinc technologies.
    Keywords: Energy Production and Conversion
    Type: NASA/CP-2000-209959 , M-963 , NAS 1.55:209959 , Aerospace Battery; Nov 16, 1999 - Nov 18, 1999; Huntsville, AL; United States
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
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    Nickel-hydrogen battery state of charge during low rate trickle charging (1996)
    In:  CASI
    Details
    Publication Date: 2019-08-15
    Description: The NASA AXAF-I program requires high battery state of charge at launch. Traditional approaches to providing high state of charge, during prelaunch operations, require significant battery cooling. The use of active cooling, in the AXAF-I prelaunch environment, was considered and proved to be difficult to implement and very expensive. Accordingly alternate approaches were considered. An approach utilizing adiabatic charging and low rate trickle charge, was investigated and proved successful.
    Keywords: Energy Production and Conversion
    Type: The 1995 NASA Aerospace Battery Workshop; 359-374; NASA-CP-3325
    Format: text
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    NASA TECHNICAL REPORTS
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