Mechanistic Insight and Optimization of Anode-Free Solid-State Batteries
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anode free batteries↗
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Results for “Engineering - Instrumentation related to nuclear science and technology”
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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Research and development of the dry tape battery concept Quarterly report no. 1, 9 Jun. - 8 Sep. 1965
Cell discharge measurements for dry tape battery couple - anode and cathode development in aqueous and nonaqueous electrolytes
CATHODE↗
Improvement in the Thermal-to-Structural Model Mapping Process for Integrated Modeling for the Roman Space Telescope
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Thermal Mapping↗
Data Driven Optimization of BN Polymer Composites Using Automated Experimentation and Machine Learning
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machine learning↗
Radiation effects on silver and zinc battery electrodes, II Interim report, Jul. - Oct. 1965
Radiation effects on silver and zinc electrodes in silver-zinc battery
STORAGE BATTERY↗
Partnerships to Advance Next Generation Manufacturing Capabilities in Support of NASA’S Exploration Goals
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additive manufacturing↗
Surface Passivation in LEO to Improve Lunar Dust Adhesion Mitigation
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Lunar Dust↗
Dynamic Regulation of Sub-Atmospheric Pressure for Constant and Cyclic Gas Loads During Testing of Spacesuit Components
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Nicholas F Materer↗
Design, Build and Qualification of 28 Volt Lithium-Ion battery
Contents include the following: 1. GSFC performance specifications requirements. 2. AEA philosophy: battery configuration. 3. AEA battery design: SONY cell, cell screening, 20Ah and 60Ah. 4. Testing: 20Ah battery qualification (environmental); 60Ah battery LEO life cycle. 5. Conclusion.: summary and lessons learned.
Curzon, D.↗
Space Shuttle News Reference
A detailed description of the space shuttle vehicle and associated subsystems is given. Space transportation system propulsion, power generation, environmental control and life support system and avionics are among the topics. Also, orbiter crew accommodations and equipment, mission operations and support, and flight crew complement and crew training are addressed.
National Aeronautics and Space Administration↗
Research and development of a high capacity, nonaqueous secondary battery Final report, Oct. 1964 - Dec. 1965
High capacity nonaqueous secondary battery
BATTERY↗
Vacuum Laser Additive Manufacturing of Lunar and Martian Regolith
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IN-situ resource untilization↗
Evaluation of Long-Term Storage Stability and Operational Efficiency of Rapid Cycle Amine Adsorbents
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John R Tidwell↗
Computer methods for the reduction correlation and analysis of space battery test data Final report, 1 May - 31 Dec. 1966
Computer methods for collection, reduction, correlation, and analysis of spacecraft nickel-cadmium battery test data
COMPUTER METHOD↗
Mars Pathfinder Lander Battery and Solar Array Performance
Mars Pathfinder Lander was powered by Ga-As solar cells and a silver-zinc Battery.
Mars↗
Chapter 3: Thermal Exchanges and Temperature Stress
Thermal comfort during space flight is discussed. Heat production of man during space flight and wear loss as a mean of dissipating heat are described. Water cooled garments are also considered, along with tolerance for extreme heat and body heat storage. Models of human temperature regulation are presented in the form of documented FORTRAN programs.
Paul Webb↗
Up-and-Coming IMCs
While the good oxidation and environmental resistance, high melting points, and comparatively low densities of such ordered intermetallics as Ti 3 Al, NiAl, FeAl, and NbAl 3 render them good candidates for advanced aerospace structures, their poor toughness at low temperatures and low strength at elevated temperatures have prompted the development of fiber-reinforced intermetallic-matrix composites (IMCs) with more balanced characteristics. Fabrication methods for continuous-fiber IMCs under development include the P/M 'powder cloth' method, the foil/fiber method, and thermal spraying. The ultimate success of IMCs depends on fibers truly compatible with the matrix materials.
Randy Bowman↗
Orbiting Solar Observatory Battery and Power Design
The OSO-1 represents a recent vintage satellite, or more recent design satellite. A summary of the battery design used on OSO-1 is presented. The temperature effects on voltage and charging-discharging of the battery system are discussed.
F E Ford↗