Silver-Zinc Battery Separator Material Development
Silver zinc battery separator material development and production
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Silver zinc battery separator material development and production
Conference on dynamics and aeroelasticity of structural materials for space shuttle design considerations
Sterilizable battery separator material preparation process
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The effect of on-line reconditioning (deep discharge) on a single, Nickel-Hydrogen spacecraft battery in GEO and LEO is considered. A life cycle test was performed in both GEO and LEO to study the effect of reconditioning on the battery's end of discharge voltage (EODV). The results of these tests show that: LEO on-line reconditioning increased the EODV (by approximately 15 cycles to maximum EODV) and the EODV lasted for approximately 300 cycles, but GEO on-line reconditioning decreased the EODV slightly during the first six days and increases significantly after the seventh day. Based on the available data from the life cycle test, it has been concluded that a long life and stable voltage is realizable with the baseline architecture (single battery, single bus) without the need for reconditioning.
Proceedings of conference on materials for improved fire safety with application to design and development of spacecraft and support equipment
Fabrication and testing of polyethylene battery separator material
Postflight analysis of parts from Surveyor 3 spacecraft, lunar material, and photographs brought back on Apollo 12 flight
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Differential drag has become a viable alternative to propulsion for satellites to avoid collisions, but there is little guidance in the literature to aid mission designers in developing a differential drag capability that verifiably meets collision avoidance efficacy standards or requirements, if such requirements were to exist. This paper proposes a differential drag efficacy determination approach based on empirical conjunctions from the NASA Conjunction Assessment Risk Analysis historical database, focusing on energy dissipation rate and change in ballistic coefficient as the key satellite parameters correlated to efficacy. The data analysis informs the discussion toward adoption of recommended differential drag requirements. A case study is presented to walk through the process to determine efficacy of a proposed mission assuming several potential requirements.
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Heat sterilizable battery separator material prepared from low-density polyethylene film
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Ethylene/acrylic acid separators for silver zinc battery applications
Ethylene/methyl acrylate copolymer synthesis for silver-zinc battery separators
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