Development of the dry tape battery concept Quarterly report no. 4, 9 Mar. - 9 Jun. 1966
Aqueous and nonqueous electrolytic actions, and energy density measurements for dry tape battery
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Aqueous and nonqueous electrolytic actions, and energy density measurements for dry tape battery
The Long Life (Lithium Ion) Battery is designed to replace the current Extravehicular Mobility Unit Silver/Zinc Increased Capacity Battery, which is used to provide power to the Primary Life Support Subsystem during Extravehicular Activities. The Charger is designed to charge, discharge, and condition the battery either in a charger-strapped configuration or in a suit-mounted configuration. This paper will provide an overview of the capabilities and systems engineering development approach for both the battery and the charger
Inorganic separator for high temperature silver-zinc battery
Filler and matrix composite materials for use in silver-zinc battery separators
Multisweep cyclic voltammetry for electrochemical characterization of systems for secondary battery application
Inorganic fillers and pressure effects on films for separators for heat sterilizable silver zinc battery
Primary zinc-silver oxide battery - separator material, construction, and prototype cell evaluation
Test of electrochemical cell and local action mechanisms of wet cell battery for space probe applications
Dry tape battery concept - cathode and anode research, energy densities, tape cell preparation, and supporting research
Silver-cadmium secondary battery energy storage system using vented cells for manned orbital spacecraft
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Computer methods for collection, reduction, correlation, and analysis of spacecraft nickel-cadmium battery test data
The NASA Aerospace Flight Battery Systems Program task status is reviewed. Major tasks incorporated in the program are battery systems, secondary batteries, and primary batteries.
High capacity nonaqueous secondary battery development - lithium deposition and cycling, ionic solvation, cathode construction and discharge efficiency, and solvent purification
Mars Pathfinder Lander was powered by Ga-As solar cells and a silver-zinc Battery.
In recent years following several spacecraft battery anomalies, it was determined that managing the operational factors of NASA flight NiCd rechargeable battery was very important in order to maintain space flight battery nominal performance. The optimization of existing flight battery operational performance was viewed as something new for a Taguchi Methods application.
Zinc-silver oxide battery design for improved and activated charge retention, voltage control, and temperature stability
Development and testing of vivyl polymer separator materials for sterilized silver-zinc secondary battery