Development of a sealed lead-acid battery for use in space Final report
Development of sealed lead-acid battery with lead- calcium grid for space application
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Development of sealed lead-acid battery with lead- calcium grid for space application
Multisweep cyclic voltammetry for electrochemical characterization of systems for secondary battery application
Active compound formation on battery nickel oxide electrode during charge, overcharge, and discharge
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Low temperature battery for space probe
The 2nd Aerospace Mechanisms Symposium, held at the University of Santa Clara on May 4-5, 1967, was sponsored by the University of Santa Clara, the Jet Propulsion Laboratory, and Lockheed Missiles and Space Company. The Symposium brought together approximately 200 representatives of more than 50 organizations concerned with mechanisms for use in space.
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Life cycle tests being run on the 50 A lightweight nickel hydrogen flight battery are discussed and the preliminary results are presented.
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Effect of radiation on nickel-cadmium battery electrodes
Quarterly Progress Report No.2: December 1st 1960 through February 28 1961
Low temperature liquid ammonia battery for space probe application
High capacity nonaqueous secondary battery
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Heat sterilizable battery separator material prepared from low-density polyethylene film