04706nam 2200601 a 450 991078154760332120230213212302.01-60086-495-31-60086-276-4(CKB)2550000000073690(EBL)3111677(SSID)ssj0001101519(PQKBManifestationID)11608291(PQKBTitleCode)TC0001101519(PQKBWorkID)11068484(PQKB)11394441(MiAaPQ)EBC3111677(Au-PeEL)EBL3111677(CaPaEBR)ebr10516782(OCoLC)922979126(EXLCZ)99255000000007369020691024d1969 uy 0engur|n|---|||||txtccrThermal design principles of spacecraft and entry bodies[electronic resource] /edited by Jerry T. BevansNew York Academic Press19691 online resource (876 p.)Progress in astronautics and aeronautics ;v. 21"A collection of technical papers drawn mainly from the AAIA 3rd Thermophysics Conference, June 24-26, 1968, subsequently revised for this volume."1-56347-870-6 Includes bibliographical references and index.""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""""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""""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""""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""""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""""Effects of Transient Pressure Environments on Heat Transfer in One-Dimensional Composite Slabs with Contact Resistance""Progress in astronautics and aeronautics ;v. 21.Space vehiclesThermodynamicsCongressesSpace vehiclesThermodynamics629.4/152Bevans Jerry T1478330American Institute of Aeronautics and Astronautics.MiAaPQMiAaPQMiAaPQBOOK9910781547603321Thermal design principles of spacecraft and entry bodies3693982UNINA