Inorganic separator for high temperature silver-zinc battery Final report, Jul. 27, 1964 - Jul. 29, 1965
Inorganic separator for high temperature silver- zinc battery
SEARCH · Search NASA
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Inorganic separator for high temperature silver- zinc battery
Inorganic separator for high temperature silver-zinc battery
Summary report is described of historical documentation and detailed design data for development of silver-zinc battery for use on Surveyor spacecraft. Electrical and physical characteristics of battery models are included, along with data on qualification, acceptance, solar-thermal-vacuum, mission simulation testing, and actual flight performance.
Silver zinc battery separator material development and production
Ethylene/acrylic acid separators for silver zinc battery applications
Remote activated silver zinc battery performance
Radiation effects on silver and zinc electrodes in silver-zinc battery
Development program for separator and modified polyethylene separator material for silver-zinc battery, and program for development of sealed heat sterilizable batteries
Development of battery terminal seal for sealing electrolyte for periods of three to five years is discussed. Operating conditions of battery are defined. Components of electrolyte seal and method of production are reported. Schematic diagrams of device are included.
Radiation effects on silver-zinc battery electrodes
Screening tests for separators in silver-zinc batteries
Development and testing of vivyl polymer separator materials for sterilized silver-zinc secondary battery
Fabrication and test of polyethylene base material for heat sterilization resistance and for battery separators in silver-zinc alkaline cell
Inorganic fillers and pressure effects on films for separators for heat sterilizable silver zinc battery
Polymer separator materials for heat sterilizable battery
Design of silver oxide-zinc battery of limited cycle life with no degradation in discharge voltage characteristics
A 45Ah Lithium ion (Li-Ion) battery comprised of 5 Yardney prismatic cells was evaluated to replace the silver-zinc cells in the Extra-vehicular Mobility Unit (EMU). Tests determined that the five cell battery can meet the mission objective of 500 duty cycles and maintain a minimum voltage of 16.0 V without an individual cell voltage dropping below 3.0V. Forty real time cycles were conducted to develop BOL trend data. Decision to switch to accelerated cycling for the remaining 460 cycles was made since Real Time cycling requires 1 day/cycle. Conclusions indicate that battery replacement would indeed be prudent.
This document contains the proceedings of the 32nd annual NASA Aerospace Battery Workshop, hosted by the Marshall Space Flight Center on November 16-18, 1999. The workshop was attended by scientists and engineers from various agencies of the US Government, aerospace contractors, and battery manufacturers, as well as international participation in like kind from a number of countries around the world. The subjects covered included nickel-hydrogen, nickel-cadmium, lithium-ion, and silver-zinc technologies.