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Entry vehicle heating and thermal protection systems [[electronic resource] ] : Space Shuttle, Solar Starprobe, Jupiter Galileo Probe / / edited by Paul E. Bauer, Howard E. Collicott



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Titolo: Entry vehicle heating and thermal protection systems [[electronic resource] ] : Space Shuttle, Solar Starprobe, Jupiter Galileo Probe / / edited by Paul E. Bauer, Howard E. Collicott Visualizza cluster
Pubblicazione: New York, N.Y., : American Institute of Aeronautics and Astronautics, c1983
Descrizione fisica: 1 online resource (588 p.)
Disciplina: 629.1 s
629.44/1
Soggetto topico: Space vehicles - Thermodynamics
Space vehicles - Atmospheric entry
Altri autori: BauerPaul E. <1924->  
CollicottHoward E  
Note generali: "Technical papers selected from the AIAA 20th Aerospace Sciences Meeting, January 1982, and the 3rd AIAA/ASME Joint Thermophysics, Fluids, Plasma, and Heat Transfer Conference, June 1982 ..."
Nota di bibliografia: Includes bibliographical references and index.
Nota di contenuto: ""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Editorial Committee""; ""List of Series Volumes""; ""Chapter I. Space Shuttle Aeroheating""; ""Aerothermodynamic Entry Environment of the Space Shuttle Orbiter""; ""Approximate Method of Predicting Heating on the Windward Side of Space Shuttle Orbiter and Comparisons with Flight Data""; ""Viscous Shock-Layer Predictions for Hypersonic Laminar or Turbulent Flows in Chemical Equilibrium over the Windward Surface of a Shuttle-Like Vehicle""
""Influence of Radiant Energy Exchange on the Determination of Convective Heat-Transfer Rates to Orbiter Leeside Surfaces during Entry""""Catalytic Efficiency of the Space Shuttle Heat Shield""; ""Catalytic Recombination/Space Shuttle Heating""; ""Viscous Shock-Layer Heating Analysis for the Shuttle Windward Symmetry Plane with Surface Finite Catalytic Recombination Rates""; ""Chapter II. Space Shuttle Thermal Protection""; ""Shuttle Orbiter Reusable Surface Insulation Thermal Performance""; ""Space Shuttle Orbiter Leading Edge Thermal Performance""
""Comparison of Orbiter STS-2 Development Flight Instrumentation Data with Thermal Math Model Predictions""""Flight Measurements of Tile Gap Heating on the Space Shuttle""; ""Tile-Gap Flow in the Shuttle Orbiter Thermal Protection System""; ""Assessment of Alternate Thermal Protection Systemsfor the Space Shuttle Orbiter""; ""Initial Shuttle External Tank Aerothermal Flight Evaluation""; ""Chapter III. Solar Starprobe Heat Shielding""; ""STARPROBE Thermal Shield System Design Concepts""; ""Preliminary Design of the Thermal Protection System for Solar Probe""
""Chapter IV. Jupiter Galileo Probe Entry Heating and Protection""""Galileo Probe Forebody Flowfield Predictions""; ""An Evaluation of Turbulence Models for Massively Blown Surfaces""; ""Trajectories of Solid Particles Spalled from a Carbonaceous Heat Shield""; ""Spallation of the Galileo Probe Heat Shield""; ""Response of Galileo Aft Cover Componentsto Laser Radiation""; ""Author Index for Volume 85""
Titolo autorizzato: Entry vehicle heating and thermal protection systems  Visualizza cluster
ISBN: 1-60086-562-3
1-60086-343-4
Formato: Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione: Inglese
Record Nr.: 9910781418003321
Lo trovi qui: Univ. Federico II
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Serie: Progress in astronautics and aeronautics ; ; v. 85.