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  • 1
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    Evaluation of positive plates with various loading levels (1977)
    In:  CASI
    Details
    Publication Date: 2006-06-18
    Description: The effects of overcharge and total cycling rate on one electrochemically impregnated and four chemically impregnated nickel electrodes are examined. Topics discussed include porosity distribution, electrode corrosion, electrolyte absorption and positive electrode involvement in the decrease in the amount of electrolyte in the separator. The electrochemically impregnated electrode is shown to be superior to all types of conventionally impregnated electrodes regardless of the loading level.
    Keywords: ENERGY PRODUCTION AND CONVERSION
    Type: NASA. Goddard Space Flight Center. The 1977 Goddard Space Flight Center Battery Workshop; p 361-376
    Format: text
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    NASA TECHNICAL REPORTS
  • 2
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    Spacecraft battery reconditioning cost considerations (1983)
    In:  CASI
    Details
    Publication Date: 2006-02-14
    Description: Cost considerations for spacecraft battery reconditioning are studied. Results indicate that the cost of performing reconditioning is minuscule compared with spacecraft system investment. Results also indicate that spacecraft life extension of a few days justifies incorporation of reconditioning circuitry.
    Keywords: ELECTRONICS AND ELECTRICAL ENGINEERING
    Type: NASA. Goddard Space Flight Center The 1982 Goddard Space Flight Center Battery Workshop; p 303-310
    Format: text
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    NASA TECHNICAL REPORTS
  • 3
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    Bipolar Nickel-hydrogen Batteries for Aerospace Applications (1984)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Description: A bipolar nickel-hydrogen battery which effectively addresses all key requirements for a spacecraft power system, including long-term reliability and low mass, is discussed. The design of this battery is discussed in the context of system requirements and nickel-hydrogen battery technology in general. To achieve the ultimate goal of an aerospace application of a bipolar Ni-H2 battery several objectives must be met in the design and development of the system. These objectives include: maximization of reliability and life; high specific energy and energy density; reasonable cost of manufacture, test, and integration; and ease in scaling for growth in power requirements. These basic objectives translate into a number of specific design requirements, which are discussed.
    Keywords: ELECTRONICS AND ELECTRICAL ENGINEERING
    Type: NASA. Goddard Space Flight Center The 1983 Goddard Space Flight Center Battery Workshop; p 495-505
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 4
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    Nickel-hydrogen batteries from Intelsat 5 to space station (1986)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Description: The heritage of the Ni-H2 technology that makes the space station application feasible is discussed. It also describes a design for a potential space station Ni-H2 battery system. Specific design values presented here were developed by Ford Aerospace as part of the Rocketdyne team effort on the Phase B Definition and Preliminary Design of the Space Station Power System in support of NASA Lewis Research Center.
    Keywords: ELECTRONICS AND ELECTRICAL ENGINEERING
    Type: NASA. Goddard Space Flight Center The 1985 Goddard Space Flight Center Battery Workshop (date); p 387 - 397
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 5
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    Energy storage systems comparison for the space station (1986)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Description: An overview of the requirements, options, selection criteria and other considerations, and current status with regard to the energy storage subsystem (ESS) for the photovoltaic power system alternative for the space station is provided.
    Keywords: ELECTRONICS AND ELECTRICAL ENGINEERING
    Type: NASA. Goddard Space Flight Center The 1985 Goddard Space Flight Center Battery Workshop (date); p 31 - 40
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 6
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    Intelsat-V: Nickel-hydrogen battery (1980)
    In:  CASI
    Details
    Publication Date: 2016-06-07
    Description: A design program for the development of a nickel hydrogen battery is described. The design and design advantages of the battery are discussed. The general characteristics of the battery such as the strain gage cell pressure monitoring and the automatic low temperature heater control are reported along with the performance characteristics.
    Keywords: ENERGY PRODUCTION AND CONVERSION
    Type: NASA. Goddard Space Flight Center The 1979 Goddard Space Flight Center Battery Workshop; p 499-513
    Format: application/pdf
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    NASA TECHNICAL REPORTS
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