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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.
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Nasa's Spacecraft Battery Evaluation Program
Acceptance testing, performance characteristics, life cycling, and failed cell analysis in NASA SPACECRAFT battery evaluation program
Development of battery separator material process Mid-program report
Heat sterilizable battery separator material prepared from low-density polyethylene film
The heat sterilizable battery.
Sealed heat sterilizable high impact resistant battery for space missions, grafting acrylic acid and polyethylene by irradiation for separator
Preparation and evaluation of fiber metal nickel battery plaques Final report, Aug. 1, 1964 - Jul. 31, 1965
Flexible fiber metal battery plaques production
The battery charger for the atmosphere Explorer B spacecraft
Battery charger for Atmosphere Explorer B spacecraft - packaging in aluminum frame rectangular configuration with three separate compartments
An averaging battery model for a lead-acid battery operating in an electric car
A battery model is developed based on time averaging the current or power, and is shown to be an effective means of predicting the performance of a lead acid battery. The effectiveness of this battery model was tested on battery discharge profiles expected during the operation of an electric vehicle following the various SAE J227a driving schedules. The averaging model predicts the performance of a battery that is periodically charged (regenerated) if the regeneration energy is assumed to be converted to retrievable electrochemical energy on a one-to-one basis.
Development of a high temperature battery first quarterly technical report
High temperature battery development - zeolites, anode and cathode couples, and molten salts
Three-day battery for 425 C environment.
Three-day battery capable of operation at temperature of 425 degrees C for use on lunar and planetary probes
Materials Challenges for Solid-State Batteries in Aerospace Applications
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Developing Low Temperature All-Solid-State-Batteries for Aerospace Applications
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Investigation of battery active nickel oxides Final report
Identification and characterization of battery active compound structures formed on nickel oxide electrode during charging and discharging
Automatic battery formation cycler and controller
Automatic battery formation cycler and controller to determine charge capacity and to perform charge-discharge operations for electrochemical cells intended for satellite power sources
Fabrication and testing of battery separator material from modified polyethylene Final report
Fabrication and testing of battery separator material of modified polyethylene film
DS2 Mars Microprobe Battery
Develop battery that will meet DS-2 power requirements under specified operational, environmental, and life requirements.
Development of a sealed lead-acid battery for use in space Final report
Development of sealed lead-acid battery with lead- calcium grid for space application
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
Lithium Battery Space Experiment
The Jet Propulsion Laboratory will test a lithium battery (Li- TiS2) in orbit and examine the battery after it is returned to Earth. The results will be used to suggest design changes for a battery that may eventually be 3-4 times lighter than the equivalent NiCd battery.