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Shuttle Orbiter Thermal Control Postflight Evaluation
Approximate Method of Predicting Heating on the Windward Side of Space Shuttle Orbiter
26 other sections not shown
0rbiter AIAA albedo antenna approximately artery axial boiloff Btu/h cabin coefficient components compressor condenser configuration contamination cooling cryogenic degradation dish DSCS DSCS III effect electronic element energy environment equinox evaluation evaporator experiment experimental facesheet finite-element flight fluid Freon gradients groove heat exchanger heat flow heat flux heat load heat pipe heat rejection Heat Transfer heat-pipe heater power honeycomb hydrogen increase input insulation interface launch LDEF liquid located loop Marangoni effect maximum membrane mission module NASA nodes operation osmotic paraffin wax payload performance power dissipation predicted pressure pump radiator reduced reflector requirements sandwich panel satellite sensor shield shown in Fig Shuttle solar array solstice solution solvent space spacecraft structure subsystem surface Table tank temperature temperature distribution thermal analysis thermal conductivity Thermal Contact Conductance thermal control thermal design thermal model Thermophysics tion transfer orbit tray tube VCHP wick