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
AIAA albedo analysis angle calculated Center chemiluminescent coating coefficient components computer-aided design COMSTAR contamination cooler curves data base degradation density developed diameter dimensionless droplets effects electrical element emissivity emitter Engineering equation factor flow flowfield fluid function geometry graphics graphite grid heat flux heat load heat pipe heat source heat transfer heat-shield heat-transfer high-temperature incident increase input interface intermediate shields material maximum measured MFHPs module monogroove NASA Navstar NEVADA node optical orbit Paper parameters particle payload performance perihelion plume predicted present primary shield problem properties radiation radiative radiosity ratio resistance roughness sample shadowing shown in Fig solar absorptance solar wind solution space spacecraft specific mass spectral structural members surface SURFACE NORMAL T₁ Teflon temperature thermal conductivity Thermal Control thermal radiation Thermionic thermocouple tion utility values vapor vector wavelength