Preliminary results from the ames emissivity experiment on oso-2.
Ames emissivity experiment on OSO-II to measure thermal radiation properties of temperature control coatings exposed to space environment
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Ames emissivity experiment on OSO-II to measure thermal radiation properties of temperature control coatings exposed to space environment
Normal spectral emittance of aluminum and zinc oxide applied to opaque substrates of different radiative properties
Cryodeposits effects on spacecraft thermal control systems with respect to surface radiative properties and to shadow shield surfaces
Ames emissivity experiment on OSO-II to measure thermal radiation properties of temperature control coatings exposed to space environment
Radiative properties of solid condensed gases with respect to cryodeposits
Thickness and space environment simulation on thermal radiation properties of high emittance ceramic and inorganic coatings for space uses
Spacecraft thermal control coating experiments, discussing unreliability of degradation results due to failure to measure radiation properties, UV wavelength dependence and micrometeroid damage
Jupiter decametric radiation properties explained by postulating inner Galilean satellite magnetic field existence
Short dipole radiation properties in lossy uniaxial medium, defining transmission parameter in terms of integrated Poynting vector
Radiation properties of shock layer and nonequilibrium flows around probes entering earth, Mars, Venus and Jupiter atmosphere
Specialists Conference held at Marshall Space Flight Center reviewed work in molecular radiation to evaluate research possibilities in this field. Topics included spectral-line studies in the labortory, application to practical heat transfer calculations of radiative transfer models, and use of measured radiation properties of gases.
Diffuse cosmic X rays from Compton collisions between galactic leakage electrons and extragalactic background photons to verify microwave blackbody radiation properties
Aerospace thermophysics considerations in spacecraft and hypervelocity vehicles systems thermal design, discussing thermal control and control coatings optical and radiative properties
Determination of correlation between impact flash radiative properties and impacting meteoroid projectile characteristics
Comparison of experimental data with predictions based on simple and more detailed models for radiation properties of surfaces
Thin metallic films thermal radiation properties at cryogenic temperatures, calculating spectral normal emissivity as temperature wavelength and thickness function
Multilayer insulation systems for cryogenics protection aboard spacecraft, considering mechanical properties, radiation shielding, component evacuation rate and outgassing
Multilayer insulation systems development and selection for cryogenics thermal protection on space vehicles, considering mechanical properties, radiation shielding, components, evacuation rate and outgassing