Electrochemical characterization of systems for secondary battery application Second quarterly report, Aug. - Oct. 1966
Multisweep cyclic voltammetry for electrochemical characterization of systems for secondary battery application
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Multisweep cyclic voltammetry for electrochemical characterization of systems for secondary battery application
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Radiation effects on silver and zinc electrodes in silver-zinc battery
Low temperature battery for space probe
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Effect of radiation on nickel-cadmium battery electrodes
Low temperature liquid ammonia battery for space probe application
Lithium-ion battery systems offer several advantages: intrinsically safe; long cycle life; environmentally friendly; high energy density; wide operating temperature range; good discharge rate capability; low self-discharge; and no memory effect.
Non-magnetic silver-cadmium battery to power apparatus on explorer 12 satellite
Heat sterilizable battery separator material prepared from low-density polyethylene film
A brief investigation of the combustion characteristics of a solid propellant containing a binder which chars, as opposed to melting or volatizing, has been made. The burning rate of the propellant with the charring binder was significantly higher than similar propellants containing non-charring binders. High speed motion pictures of the burning propellant showed that the aluminum burned on the regressing surface, rather than a short distance from it as is typical with composite propellants.
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Mars Pathfinder Lander was powered by Ga-As solar cells and a silver-zinc Battery.
Solar power system for the ariel satellite /uk-1/
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