Entry vehicle heating and thermal protection systems [[electronic resource] ] : Space Shuttle, Solar Starprobe, Jupiter Galileo Probe / / edited by Paul E. Bauer, Howard E. Collicott |
Pubbl/distr/stampa | 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 |
Altri autori (Persone) |
BauerPaul E. <1924->
CollicottHoward E |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Space vehicles - Thermodynamics
Space vehicles - Atmospheric entry |
Soggetto genere / forma | Electronic books. |
ISBN |
1-60086-562-3
1-60086-343-4 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
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"" |
Record Nr. | UNINA-9910457235603321 |
New York, N.Y., : American Institute of Aeronautics and Astronautics, c1983 | ||
![]() | ||
Lo trovi qui: Univ. Federico II | ||
|
Entry vehicle heating and thermal protection systems [[electronic resource] ] : Space Shuttle, Solar Starprobe, Jupiter Galileo Probe / / edited by Paul E. Bauer, Howard E. Collicott |
Pubbl/distr/stampa | 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 |
Altri autori (Persone) |
BauerPaul E. <1924->
CollicottHoward E |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Space vehicles - Thermodynamics
Space vehicles - Atmospheric entry |
ISBN |
1-60086-562-3
1-60086-343-4 |
Formato | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
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"" |
Record Nr. | UNINA-9910781418003321 |
New York, N.Y., : American Institute of Aeronautics and Astronautics, c1983 | ||
![]() | ||
Lo trovi qui: Univ. Federico II | ||
|