Spacecraft radiative transfer and temperature control
American Institute of Aeronautics and Astronautics, 1982 - Technology & Engineering - 529 pages
Good,No Highlights,No Markup,all pages are intact, Slight Shelfwear,may have the corners slightly dented, may have slight color changes/slightly damaged spine.
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Effects of Polarization on Bidirectional Reflectance
Determination of Radiative Properties from Transport Theory
Melting of a Slab of Semitransparent Material by Irradiation
23 other sections not shown
AIAA albedo analysis angle approximately calculated Center chemiluminescent coating coefficient comparison components computer-aided design COMSTAR conductively coupled constant contamination cooler coordinate curves degradation density developed diameter dimensionless droplets effects electrical resistivity emission emitter energy Engineering equation factor flow flowfield fluid function geometry graphics graphite grid heat flux heat pipe heat source heat transfer heat-shield heat-transfer high-temperature incident increase input interactive interface intermediate shields mass loss material maximum measured MFHPs module monogroove NASA NEVADA node optical orbit Paper parameters particle payload performance perihelion plume predicted present primary shield problem properties radiation radiosity ratio resistance sample shadowing shown in Fig silica solar absorptance solar wind solution space spacecraft specific mass spectral structural members surface Table Teflon temperature thermal conductivity Thermal Control thermal radiation Thermionic thermocouple Thermophysics tion utility values vapor vector wavelength