Thermophysics of Spacecraft and Outer Planet Entry Probes: Technical Papers Selected from AIAA 14th Aerospace Sciences Meeting, January 1976, and the AIAA 11th Thermophysics Conference, July 1976 (with One Exception), Subsequently Revised for this VolumeAllie M. Smith, American Institute of Aeronautics and Astronautics |
Contents
Development of PhaseChange Systems | 19 |
Analysis of Axially Grooved HeatPipe Condensers | 37 |
GradedPorosity HeatPipe Wicks | 57 |
Copyright | |
19 other sections not shown
Common terms and phrases
ablation AIAA AIAA Paper analysis approximately atmosphere axial ballistic coefficient blade calculated carbon condensation cone half-angle configuration constriction resistance contact area convective convective heating cool coupled cryofilms crystal decrease dimensionless distribution drag coefficient engine entry probe equation exhaust plume experimental flow flowfield FRSI panel graphite groove heat flux heat pipe heat shield heat transfer heat-transfer heating environment hyperboloid incidence angles increase initial integral liquid louver mass loss material maximum measured melting microbalance NASA nose O/F ratio obtained optical outgassing outgassing rate parameter phase-change porosity presented in Fig problem radiant intensity radiation radiative heating rate radiative transfer region rocket Saturn shape change shock layer shown in Fig silica solar absorptance solution species spectral specular sphere cone stagnation point surface temperature thermal conductivity Thermophysics tion Uranus vapor pressure velocity wick