Apparatus to measure the mid-infrared spectral emittance of cold powders in a vacuum
Apparatus for measuring mid-infrared spectral emission from cold powders in vacuum
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Apparatus for measuring mid-infrared spectral emission from cold powders in vacuum
Computer analysis of curve for total emission from group of separate localized emission points on surface of high vacuum metallic cathode
Reflectance, transmittance and absorptance of muscovite type mica as function of thickness measured, using prism and grating spectrophotometers
Spectral emission and radiance calculations for solid rocket propellant plumes
Optical properties and stability of vacuum deposited silver and dielectric film coatings
Reflectance, transmittance and absorptance of muscovite type mica as function of thickness measured, using prism and grating spectrophotometers
Preferred crystal orientations and vacuum work functions of planar tungsten deposits formed by hydrogen reduction of tungsten chloride
Dielectric films used for thermal radiation control coatings
Solar absorptance and hemispherical emmitance of metals at space conditions determined with cyclic incident radiation technique
Performance of deposited tungsten as thermionic converter
Photoelectron spectroscopy energy analyzer with spherical retarding field screen, discussing electronic circuit configuration, operational characteristics and spectral resolution
Field ionization yield with single graphite whisker lateral surface as ionizer, using helium, ammonia, carbon monoxide and carbon dioxide
The 18-cm microwave spectra of Orion B and W3A show evidence of an emission feature to the high-frequency side of the carbon recombination line. Observations at different frequencies establish that this feature results from electronic recombination. In addition, theoretical considerations, results of 21-cm observations, and computer-simulated spectra suggest that the new feature originates in a predominantly neutral hydrogen region and can be explained by a superposition of recombination lines from any or all of the following elements: Mg-24, Si-28, S-32, and Fe-56.
Coated surface withstands space environment with negilgible change in radiation characteristics and physical properties. Process can be used with any porous substance, as long as pores are large enough to allow molecules of reacting solutions to enter and yet not so large as to allow nickel sulfide to be leached out of pores before sealing.
Simultaneous measurements were made on three surface insulation coatings for total surface radiation and radiation at discrete wavelengths between 0.88 and 4.5 microns. The mullite coating radiated all the applied heat at convective heat rates of 204 and 295 kw/sq m. Radiation from the ceramic mullite fiber coating was 170 kw/sq m at a heat rate of 454 kw/sq m. Effective total emissivity and spectral emissivity values were evaluated; all three coatings were significantly non-grey. Effective total emissivity values were 0.79 for mullite, 0.50 for ceramic mullite fiber, and 0.78 for silica composite.
The surface regions of a DSNiCrAl alloy have been doped, by a pack diffusion process, with small amounts of Mn, Fe, or Co, and the effect of these dopants on the total normal emissivity of the scales produced by subsequent high temperature oxidation has been measured. While all three elements lead to a modest increase in emissivity, (up to 23% greater than the undoped alloy) only the change caused by manganese is thermally stable. However, this increased emissivity is within 85 percent of that of TDNiCr oxidized to form a chromia scale. The maganese-doped alloy is some 50 percent weaker than undoped DSNiCrAl after the doping treatment, and approximately 30 percent weaker after oxidation.
Testing of two fuel clad specimens for thermionic reactor application is described. The annular UO2 fuel was clad on both sides with tungsten; heat rejection was radially inward. The tests were intended to study inner clad stability, fuel redistribution, and fuel melting problems. The specimens were tested in a vacuum chamber using electron bombardment heating. Fuel structural changes were studied using periodic gammagraphs and posttest metallography. The first specimen test was terminated at 50 hours because of a braze failure. The second specimen was tested for 240 hours when an outer clad leak developed due to a tungsten-water reaction. The fuel developed numerous cracks on cooldown but the inner clad remained dimensionally stable. The fuel cover gas did not impede the rate of fuel redistribution. Posttest examination showed the fuel had not melted during operation.
Results from tests of the first variable-gap diminiode at an initial interelectrode spacing of 0.23 millimeter indicate sharply defined, relatively low ultimate power points. This characteristic supports the value of the diminiode as a well-controlled tool for thermionic-conversion research and development.