Development of battery separator material process Interim report
Sterilizable battery separator material preparation process
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Sterilizable battery separator material preparation process
Development program for separator and modified polyethylene separator material for silver-zinc battery, and program for development of sealed heat sterilizable batteries
Screening tests for separators in silver-zinc batteries
Inorganic separator for high temperature silver- zinc battery
Fabrication and testing of polyethylene battery separator material
Active compound formation on battery nickel oxide electrode during charge, overcharge, and discharge
Future cryogenic propulsion systems will require efficient methods with which to transfer cryogenic propellants from a depot storage tank to a customer receiver tank to minimize cost and maximize reusability. The Reduced Gravity Cryogenic Transfer project is currently developing advanced cryogenic fluid management technology and developing and validating new numerical models for three phases of transfer: line chilldown, tank chilldown, and tank fill. Additionally, multiple liquid nitrogen (LN 2 ) parabolic flight transfer rigs are being designed by universities and NASA to investigate the gravitational sensitivities that exist in these three technologies. In order to maximize the collection of low-g data during flights, it is required to extract as much (LN 2 as possible from the supply tank, despite variable gravity levels. The purpose of this paper is to present computational fluid dynamics (CFD) volume of fluid simulations of (LN 2 behavior in the supply tank onboard parabolic flights to validate the optimal design of a bi-directional propellant management device (PMD) using the commercial software FLOW-3D. A parametric study is conducted on the effects of gravity level, fill level, pore size, open area, thickness, and type of baffle on PMD performance. Based on results, the PMD as designed exceeds the targeted expulsion efficiency.
Low temperature battery for space probe
Computer programs for processing and analyzing nickel-cadmium battery and time-dependent data
Lithium and copper electrode studies in research and development of high capacity nonaqueous secondary battery
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