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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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Thermal insulation technique permits low and high power electronic chips to operate in the same package without thermal cross-coupling. An alumina glass shield thermally isolates the low power chip from the high power chip while Kovar substrate acts as a heat sink to remove heat from the high power chip.
Ceramic composite thermal insulation comprised of alumina-silica fibers, pigmentary potassium titanate, and asbestos fibers, bonded with a colloidal silica sol has improved insulating capabilities to both radiant and convective heat. Gelation of the colloidal silica sol prevents binder migration.
Thermal insulation for extravehicular space suits
Development of thermal insulation material for insulating liquid hydrogen tanks in spacecraft
Thermal insulation and structural support for thermoelectric devices, discussing fabrication of diffusion bonded structures in conjunction with material selection
Long term vacuum storage test and vibration effects analysis of multilayer super insulation blankets
Ceramic composite thermal insulations for launch vehicle radiant heating environments
Low density thermal insulation materials for use above 3000-deg f
Comparison of stitched foam thermal insulation protection system for liquid hydrogen tank wall of Centaur launch vehicle with ac-6 jettisonable insulation
Effective thermal insulation characteristics of interstitial materials under compression loads and varying temperatures
Tests and analyses to select materials and techniques for thermal insulation of planetary spacecraft
Cylindrical calorimeter designed to measure temperature dependent thermal conductivity for high performance insulation
Ceramic foam as lightweight thermal insulation for rigid heat shields in launch vehicles
Foamed refractory oxides provide lightweight, reflective thermal insulation materials. The materials have a low bulk density and high thermal shock resistance.
Moisture detector for evaluating trapped water effects in thermal insulation, describing equipment and test procedure
Optimized zirconia foam ceramic body shows promise for use as a thermal insulation material. The insulating media displays low density and thermal conductivity, good thermal shock resistance, high melting point, and mechanical strength.
Zirconium oxide polycrystalline fibers for improving structural rigidity and thermal insulation of zirconium oxide foam
Spray-on process constructs molds used in forming sections of thermal insulation blankets. The process simplifies the fabrication of blankets by eliminating much of the equipment formerly required and decreasing the time involved.