3 pages matching spacecraft skin temperature in this book
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apparent absorptance apparent emittance base plate basic bimetallic Btu/hr calculated Cat-a-lac white paint configuration factors contact cement covered with aluminum covered with Saureisen crossbow curvature curves determined Effective Reflectance Ratio energy exchange energy flux energy input energy loss evaluation experimental F22 tot Figure 11 Figure 17 fin inner surface fin material given by equation heat source heat treatment high-expansion side inches infinite length Invar K25 rad K34 rad mandrel manganese metal wall container NASA CR-9I ref node normal incidence obtained open position outer surface parallel plates power dissipation Radiant Energy radiant transfer functions Reflectance Ratio H/W shown in Figure slots solar absorptance Solar Constant solar energy absorbed solar input solar irradiation Solar Polar Angle solar simulator spacecraft skin temperature spacecraft surface specular V-groove styrofoam system is shown technique terrestial emittance Test Number test section test surface thermal analysis thermal conductance Thermal Model thermocouples typical fin values