USE OF A SEALED SILVER CADMIUM BATTERY ON EXPLORER XII
Use of a sealed silver cadmium battery on explorer xii
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Use of a sealed silver cadmium battery on explorer xii
Low temperature liquid ammonia battery for space probe application
Nickel-cadmium spacecraft battery with auxiliary charge control electrode
Low temperature battery - development of pasted plate cathode construction to extend cell life
High capacity nonaqueous secondary battery
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Non-magnetic silver-cadmium battery to power apparatus on explorer 12 satellite
Acceptance testing, performance characteristics, life cycling, and failed cell analysis in NASA SPACECRAFT battery evaluation program
Heat sterilizable battery separator material prepared from low-density polyethylene film
Sealed heat sterilizable high impact resistant battery for space missions, grafting acrylic acid and polyethylene by irradiation for separator
Flexible fiber metal battery plaques production
Performance of a sealed-silver cadmium battery on explorer xii
Battery charger for Atmosphere Explorer B spacecraft - packaging in aluminum frame rectangular configuration with three separate compartments
A battery model is developed based on time averaging the current or power, and is shown to be an effective means of predicting the performance of a lead acid battery. The effectiveness of this battery model was tested on battery discharge profiles expected during the operation of an electric vehicle following the various SAE J227a driving schedules. The averaging model predicts the performance of a battery that is periodically charged (regenerated) if the regeneration energy is assumed to be converted to retrievable electrochemical energy on a one-to-one basis.
High temperature battery development - zeolites, anode and cathode couples, and molten salts
Radiation effects on silver and zinc battery electrodes
X-ray diffraction patterns of nickel-cadmium battery electrodes and stabilization of nickel oxides and hydroxides