Spacecraft Radiative Transfer and Temperature ControlThomas E. Horton 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. |
Contents
Effects of Polarization on Bidirectional Reflectance | 3 |
Determination of Radiative Properties from Transport Theory | 22 |
Melting of a slab of Semitransparent Material by Irradiation | 38 |
Copyright | |
23 other sections not shown
Common terms and phrases
absorption AIAA analysis angle applications approximately assumed base calculated Center coating coefficient comparison components conductivity constant converter cooler curves determined developed direction distribution effects electrical element emissivity energy Engineering equation experiment factor flow function geometry given graphics heat flux heat pipe heat transfer incident increase input interface internal length limited liquid load loss mass material maximum means measured method module normal obtained optical orbit parameters particle performance plume predicted present pressure primary problem properties radiation radiative range ratio reflectance relative Research resistance respectively roughness sample shadowing shield shown in Fig shows solar solid solution space spacecraft specific spectral structural surface Table Teflon temperature thermal tion utility values vapor wall wavelength