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Entry Vehicle Heating and Thermal Protection Systems : Space Shuttle, Solar Starprobe, Jupiter Galileo Probe.

By: Contributor(s): Material type: TextTextSeries: Progress in Astronautics and AeronauticsPublisher: Reston : American Institute of Aeronautics and Astronautics, 1983Copyright date: ©1983Edition: 1st edDescription: 1 online resource (588 pages)Content type:
  • text
Media type:
  • computer
Carrier type:
  • online resource
ISBN:
  • 9781600863431
Subject(s): Genre/Form: Additional physical formats: Print version:: Entry Vehicle Heating and Thermal Protection SystemsDDC classification:
  • 629.1 s;629.44/1
LOC classification:
  • TL900 -- .A33 1982eb
Online resources:
Contents:
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.
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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.

Description based on publisher supplied metadata and other sources.

Electronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2024. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.

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