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Record Nr. |
UNINA9910781547603321 |
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Titolo |
Thermal design principles of spacecraft and entry bodies [[electronic resource] /] / edited by Jerry T. Bevans |
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Pubbl/distr/stampa |
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New York, : Academic Press, 1969 |
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ISBN |
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1-60086-495-3 |
1-60086-276-4 |
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Descrizione fisica |
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1 online resource (876 p.) |
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Collana |
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Progress in astronautics and aeronautics ; ; v. 21 |
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Altri autori (Persone) |
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Disciplina |
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Soggetti |
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Space vehicles - Thermodynamics |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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"A collection of technical papers drawn mainly from the AAIA 3rd Thermophysics Conference, June 24-26, 1968, subsequently revised for this volume." |
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Nota di bibliografia |
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Includes bibliographical references and index. |
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Nota di contenuto |
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""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 |
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