Prospects for Implementing Variable Emittance Thermal Control of Space Suits on the Martian Surface
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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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Spectral emission from refractory oxides at high temperatures
Shallow reference cavities for high temperature emission measurements
Electron emission test of uranium carbide compatibility with tungsten alloys for nuclear fuel elements
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Test of analytical expressions for thermal emission of shallow cylindrical cavities using spectrophotometer
Effect of surface roughness, damage, and films on thermal emission
Effect of slight surface roughness on thermal emission
Time variation of total hemispherical emission of polished platinum surfaces at high temperatures
Effects of evaporation rate and oxygen pressure on characteristics of silicon oxide films, and angular reflectance of metals determined by optical constants
Rotating cylinder equipment for measuring total and spectral normal emission of metals and nonmetals over temperature range of 1200 to 1800 deg K
Hemispherical spectral emission of ablation chars, carbon, and zirconium oxide formed during reentry
Apparatus for measuring emission of organic materials
Heat conductive loss along supporting wires, air conductive loss in evacuated chamber - loss corrections for hemispherical emission measurements by decay method
Application of temperature rate measurements to determination of thermal emission of spacecraft temperature control surfaces
Effect of absorptance/emittance ratio on storage of cryogenic propellants in deep space
Electroluminescent materials for spacecraft temperature control
Development of space stable thermal control coatings