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
|
| 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 | |
| Soggetto genere / forma: | Electronic books. |
| 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 |
| ISBN: | 1-60086-562-3 |
| 1-60086-343-4 | |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910457235603321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |
Serie:
Progress in astronautics and aeronautics ; ; v. 85.