Spacecraft Thermal Control, Design, and OperationHoward E. Collicott, Paul E. Bauer |
Contents
The Evolving | 3 |
Shuttle Orbiter Thermal Control Postflight Evaluation | 17 |
Approximate Method of Predicting Heating on the Windward Side of Space Shuttle Orbiter | 21 |
Copyright | |
29 other sections not shown
Common terms and phrases
absorptance AIAA antenna approximately artery axial boiloff boundary Btu/h cabin coefficient components compressor condenser contaminated control volume cooling cryogenic degradation DSCS DSCS III effect energy equations equinox evaluated evaporator experiment experimental FACESHEET finite elements finite-element flight fluid formulation Freon 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 loop Marangoni effect maximum membrane mission module NASA nodes operation orbit osmotic paraffin wax payload performance predicted pressure problem pump radiator reduced reflector requirements sandwich panel satellite sensor shield shown in Fig Shuttle solar array solution solvent space spacecraft structural subelement subsystem surface Table tank temperature temperature distribution thermal analysis thermal conductivity Thermal Contact Conductance thermal control thermal design thermal model Thermophysics tion TPS/structural transient transport capacity tray tube valve VCHP wick