04489nam 2200661 a 450 991045723560332120200520144314.01-60086-562-31-60086-343-4(CKB)2550000000073443(EBL)3111587(SSID)ssj0000565891(PQKBManifestationID)12252128(PQKBTitleCode)TC0000565891(PQKBWorkID)10533750(PQKB)10688386(MiAaPQ)EBC3111587(Au-PeEL)EBL3111587(CaPaEBR)ebr10516691(OCoLC)922978977(EXLCZ)99255000000007344319830712d1983 uy 0engur|n|---|||||txtccrEntry vehicle heating and thermal protection systems[electronic resource] Space Shuttle, Solar Starprobe, Jupiter Galileo Probe /edited by Paul E. Bauer, Howard E. CollicottNew York, N.Y. American Institute of Aeronautics and Astronauticsc19831 online resource (588 p.)Progress in astronautics and aeronautics ;v. 85"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 ..."0-915928-74-4 Includes bibliographical references and index.""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""Progress in astronautics and aeronautics ;v. 85.Space vehiclesThermodynamicsCongressesSpace vehiclesAtmospheric entryCongressesElectronic books.Space vehiclesThermodynamicsSpace vehiclesAtmospheric entry629.1 s629.44/1Bauer Paul E.1924-954730Collicott Howard E954731American Institute of Aeronautics and Astronautics.American Society of Mechanical Engineers.AIAA/ASME Joint Thermophysics, Fluids, Plasma, and Heat Transfer Conference(3rd :1982 :Saint Louis, Mo.)MiAaPQMiAaPQMiAaPQBOOK9910457235603321Entry vehicle heating and thermal protection systems2159455UNINA