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100   $a20691024d1969      uy             0
101 0 $aeng
135   $aur|n|---|||||
181   $ctxt
182   $cc
183   $acr
200 10$aThermal design principles of spacecraft and entry bodies$b[electronic resource] /$fedited by Jerry T. Bevans
210   $aNew York $cAcademic Press$d1969
215   $a1 online resource (876 p.)
225 1 $aProgress in astronautics and aeronautics ;$vv. 21
300   $a"A collection of technical papers drawn mainly from the AAIA 3rd Thermophysics Conference, June 24-26, 1968, subsequently revised for this volume."
311   $a1-56347-870-6 
320   $aIncludes bibliographical references and index.
327   $a""COVER""; ""TITLE""; ""COPYRIGHT""; ""THE THERMOPHYSICS COMMITTEE, 1967 and 1968""; ""PREFACE""; ""EDITORIAL COMMITTEE FOR VOLUME 21""; ""CONTENTS""; ""I. THERMAL PROCESSES AND THERMAL DESIGN""; ""I.I Thermal Analysis""; ""Higher-Order Approximations for Lumped System Analysis of Evacuated Enclosures""; ""Optical Measurements of the Radiation Configuration Factor""; ""Optical Shape Factor Data Processing through Computer Graphics""; ""An Experimental Technique for Measuring Local Solar Irradiation with a Model Spacecraft""
327   $a""An Approximate Analytic Solution of the Steady-State Thermal Design Problem of Space Radiators""""I.2 Entry Heating: Convection, Radiation, and Ablation""; ""Radiative Transport in Inviscid Nonadiabatic Stagnation-Region Shock Layers""; ""Radiation Transfer through High-Temperature Shock Layers""; ""Remote Sensing of Rarefied Gas Flows through a Fluorescence Technique""; ""Thermodynamic Performance of Carbon in Hyperthermal Environments""; ""A Rapid Technique for Estimating Ablative Heat Shield Weights from Plasma Jet Test Data""
327   $a""Surface Oxidation with Streamwise Variation of Wall Reactivity""""Hypersonic, Diffusion-Controlled Oxidation of Tungsten""; ""I.3 Rocket Exhaust Effects""; ""Spectral Radiance of Model Rocket Exhaust Plumes at High Altitudes""; ""Effects of the LM Descent Engine Exhaust on Lunar Surface Temperatures""; ""I.4 Lunar and Planetary Vehicles Design""; ""A Study of the Thermal Kill of Viable Organisms during Mars Atmospheric Entry""; ""Prediction of the Martian Thermal Environment""; ""Thermal Control Aspects of a Stationary Martian Surface Laboratory""
327   $a""Thermal Testing under Simulated Martian Environment""""LM Passive Thermal Design and Test""; ""II. THERMOPHYSICAL PROPERTIES FOR DESIGN""; ""II. 1 Remote Measurements""; ""Determination of Optical and Physical Properties of Artificial Satellites by Passive Ground-Based Photometry""; ""Predicting Lunar Temperatures""; ""Lunar Surface Thermal Characteristics during Eclipse from Surveyors III, V and after Sunset from Surveyor V""; ""II.2 Thermal Radiation Properties""; ""Emission, Total Internal Reflection, and Tunneling of Thermal Radiation in Metals""
327   $a""Measurements of Thermal Radiation of Solids at Liquid-Helium Temperatures""""A Technique for the Measurement of Spectral Reflectances at Low Temperatures in the Infrared and Far Infrared""; ""Development of Phase-Change Coatings""; ""II.3 Joint Conductance""; ""Simultaneous Radiation and Conduction between Rough Surfaces""; ""Thermal Conductance of Two-Dimensional Constrictions""; ""An Exact Solution for Thermal Conduction through a Two- Dimensional Eccentric Constriction""
327   $a""Effects of Transient Pressure Environments on Heat Transfer in One-Dimensional Composite Slabs with Contact Resistance""
410  0$aProgress in astronautics and aeronautics ;$vv. 21.
606   $aSpace vehicles$xThermodynamics$vCongresses
615  0$aSpace vehicles$xThermodynamics
676   $a629.4/152
701   $aBevans$b Jerry T$01478330
712 02$aAmerican Institute of Aeronautics and Astronautics.
801  0$bMiAaPQ
801  1$bMiAaPQ
801  2$bMiAaPQ
906   $aBOOK
912   $a9910781547603321
996   $aThermal design principles of spacecraft and entry bodies$93693982
997   $aUNINA