Thermal design principles of spacecraft and entry bodies [[electronic resource] /] / edited by Jerry T. Bevans

• Pubblicazione: New York, : Academic Press, 1969
• Descrizione fisica: 1 online resource (876 p.)
• Disciplina: 629.4/152
• Soggetto topico: Space vehicles - Thermodynamics
• Altri autori: BevansJerry T
• Note generali: "A collection of technical papers drawn mainly from the AAIA 3rd Thermophysics Conference, June 24-26, 1968, subsequently revised for this volume."
• Nota di bibliografia: Includes bibliographical references and index.
• Nota di contenuto: ""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""
• Titolo autorizzato: Thermal design principles of spacecraft and entry bodies
• ISBN: 1-60086-495-3; 1-60086-276-4
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910781547603321
• Lo trovi qui: Univ. Federico II
• Serie: Progress in astronautics and aeronautics ; ; v. 21.