Thermal design principles of spacecraft and entry bodies [[electronic resource] /] / edited by Jerry T. Bevans
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| Titolo: |
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 |
| Opac: | Controlla la disponibilità qui |
Serie:
Progress in astronautics and aeronautics ; ; v. 21.