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Aerospace thermal structures and materials for a new era [[electronic resource] /] / edited by Earl A. Thornton
| Aerospace thermal structures and materials for a new era [[electronic resource] /] / edited by Earl A. Thornton |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 1995 |
| Descrizione fisica | 1 online resource (400 pages) : illustrations |
| Altri autori (Persone) | ThorntonEarl A |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico | Space vehicles - Thermodynamics |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-636-0
1-60086-417-1 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Preface""; ""Table of Contents""; ""Chapter 1. Analysis of Thermal Structures""; ""Numerical Modeling of a Cryogenic Fluid within a Fuel Tank""; ""Thermocryogenic Buckling and Stress Analyses of a Partially Filled Cryogenic Tank Subjected to Cylindrical Strip Heating""; ""Random Vibration of Thermally Buckled Plates""; ""On Thermally-Induced Vibrations of Structures in Space""; ""Transient Thermal-Structural Response of a Space Structure with Thermal Control Materials""; ""Chapter 2. Experimental Studies of Thermal Structures""
""Boundary Conditions for Aerospace Thermal-Structural Tests""""Inverse Analysis for Structural Boundary Condition Characterization of a Panel Test Fixture""; ""An Experimental Investigation of Thermally Induced Vibrations of Spacecraft Structures""; ""Chapter 3. Analysis of High Temperature Compsosites""; ""Recent Advances in the Mechanics of Functionally Graded Compsosites""; ""Micromechanical Analysis of Thermal Response in Textile-Based Compsosites""; ""Recent Advances in the Sensitivity Analysis for the Thermomechanical Postbuckling of Composites Panels"" ""Laser Induced Thermal Stresses in Composite Materials""""Quantification of Uncertainties of Hot-Wet Composite Long Term Behavior""; ""Minimizing Thermal Deformation by Using Layered Structures""; ""Harmonic Generalized Thermoelastic Waves in Anisotropic Laminated Compsosites""; ""The Superplastic Deformation Behavior of Physical Vapor Deposited Ti-6Al-4V""; ""Chapter 4. Performance of Aircraft Materials""; ""Aluminum Alloys for Subsonic Aircraft""; ""Materials Requirements for Aircraft Engines""; ""Benefits Estimation of New Engine Technology Insertion""; ""Author Index for Volume"" |
| Record Nr. | UNINA-9910457199103321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 1995 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aerospace thermal structures and materials for a new era [[electronic resource] /] / edited by Earl A. Thornton
| Aerospace thermal structures and materials for a new era [[electronic resource] /] / edited by Earl A. Thornton |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 1995 |
| Descrizione fisica | 1 online resource (400 pages) : illustrations |
| Altri autori (Persone) | ThorntonEarl A |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico | Space vehicles - Thermodynamics |
| ISBN |
1-60086-636-0
1-60086-417-1 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Preface""; ""Table of Contents""; ""Chapter 1. Analysis of Thermal Structures""; ""Numerical Modeling of a Cryogenic Fluid within a Fuel Tank""; ""Thermocryogenic Buckling and Stress Analyses of a Partially Filled Cryogenic Tank Subjected to Cylindrical Strip Heating""; ""Random Vibration of Thermally Buckled Plates""; ""On Thermally-Induced Vibrations of Structures in Space""; ""Transient Thermal-Structural Response of a Space Structure with Thermal Control Materials""; ""Chapter 2. Experimental Studies of Thermal Structures""
""Boundary Conditions for Aerospace Thermal-Structural Tests""""Inverse Analysis for Structural Boundary Condition Characterization of a Panel Test Fixture""; ""An Experimental Investigation of Thermally Induced Vibrations of Spacecraft Structures""; ""Chapter 3. Analysis of High Temperature Compsosites""; ""Recent Advances in the Mechanics of Functionally Graded Compsosites""; ""Micromechanical Analysis of Thermal Response in Textile-Based Compsosites""; ""Recent Advances in the Sensitivity Analysis for the Thermomechanical Postbuckling of Composites Panels"" ""Laser Induced Thermal Stresses in Composite Materials""""Quantification of Uncertainties of Hot-Wet Composite Long Term Behavior""; ""Minimizing Thermal Deformation by Using Layered Structures""; ""Harmonic Generalized Thermoelastic Waves in Anisotropic Laminated Compsosites""; ""The Superplastic Deformation Behavior of Physical Vapor Deposited Ti-6Al-4V""; ""Chapter 4. Performance of Aircraft Materials""; ""Aluminum Alloys for Subsonic Aircraft""; ""Materials Requirements for Aircraft Engines""; ""Benefits Estimation of New Engine Technology Insertion""; ""Author Index for Volume"" |
| Record Nr. | UNINA-9910781407503321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 1995 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aerospace thermal structures and materials for a new era [[electronic resource] /] / edited by Earl A. Thornton
| Aerospace thermal structures and materials for a new era [[electronic resource] /] / edited by Earl A. Thornton |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 1995 |
| Descrizione fisica | 1 online resource (400 pages) : illustrations |
| Altri autori (Persone) | ThorntonEarl A |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico | Space vehicles - Thermodynamics |
| ISBN |
1-60086-636-0
1-60086-417-1 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Preface""; ""Table of Contents""; ""Chapter 1. Analysis of Thermal Structures""; ""Numerical Modeling of a Cryogenic Fluid within a Fuel Tank""; ""Thermocryogenic Buckling and Stress Analyses of a Partially Filled Cryogenic Tank Subjected to Cylindrical Strip Heating""; ""Random Vibration of Thermally Buckled Plates""; ""On Thermally-Induced Vibrations of Structures in Space""; ""Transient Thermal-Structural Response of a Space Structure with Thermal Control Materials""; ""Chapter 2. Experimental Studies of Thermal Structures""
""Boundary Conditions for Aerospace Thermal-Structural Tests""""Inverse Analysis for Structural Boundary Condition Characterization of a Panel Test Fixture""; ""An Experimental Investigation of Thermally Induced Vibrations of Spacecraft Structures""; ""Chapter 3. Analysis of High Temperature Compsosites""; ""Recent Advances in the Mechanics of Functionally Graded Compsosites""; ""Micromechanical Analysis of Thermal Response in Textile-Based Compsosites""; ""Recent Advances in the Sensitivity Analysis for the Thermomechanical Postbuckling of Composites Panels"" ""Laser Induced Thermal Stresses in Composite Materials""""Quantification of Uncertainties of Hot-Wet Composite Long Term Behavior""; ""Minimizing Thermal Deformation by Using Layered Structures""; ""Harmonic Generalized Thermoelastic Waves in Anisotropic Laminated Compsosites""; ""The Superplastic Deformation Behavior of Physical Vapor Deposited Ti-6Al-4V""; ""Chapter 4. Performance of Aircraft Materials""; ""Aluminum Alloys for Subsonic Aircraft""; ""Materials Requirements for Aircraft Engines""; ""Benefits Estimation of New Engine Technology Insertion""; ""Author Index for Volume"" |
| Record Nr. | UNINA-9910809690203321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 1995 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Basic research and technologies for two-state-to-orbit vehicles [[electronic resource] ] : final report of the collaborative research centres / / edited by Dieter Jacob, Gottfried Sachs and Siegfried Wagner
| Basic research and technologies for two-state-to-orbit vehicles [[electronic resource] ] : final report of the collaborative research centres / / edited by Dieter Jacob, Gottfried Sachs and Siegfried Wagner |
| Pubbl/distr/stampa | Weinheim, : Wiley-VCH, c2005 |
| Descrizione fisica | 1 online resource (686 p.) |
| Disciplina |
629.4
629.47 |
| Altri autori (Persone) |
JacobDieter <1941->
SachsG (Gottfried) WagnerS <1937-2018.> (Siegfried) |
| Collana | Deutsche Forschung |
| Soggetto topico |
Space vehicles - Aerodynamics
Space vehicles - Design and construction Space vehicles - Materials Space vehicles - Thermodynamics |
| ISBN |
1-280-52056-6
9786610520565 3-527-60571-1 3-527-60550-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Basic Research and Technologies for Two-Stage-to-Orbit Vehicles; Contents; 1 Introduction; 2 Network Organization of Collaborative Research Centres for Scientific Efficiency Enhancement; 2.1 Introduction; 2.2 Organization of Collaboration; 2.3 Efficiency Enhancement in Research; 2.4 Efficiency Enhancement in Teaching and Education; 2.5 Internationalization; 2.6 Final Remarks; 3 Overall Design Aspects; 3.1 Conceptual Design of Winged Reusable Two-Stage-to-Orbit Space Transport Systems; 3.1.1 Background and Introduction; 3.1.2 Concepts for Reusable Space Transports
3.1.2.1 Single-Stage-to-Orbit SSTO3.1.2.2 Two-Stage-to-Orbit TSTO; 3.1.3 Design Procedure; 3.1.3.1 Design Tools and Methods; 3.1.3.2 Baseline Concept; 3.1.3.3 Boundary Conditions and Requirements; 3.1.3.4 Variation of Mission and Staging Mach Number; 3.1.3.5 Trade Studies; 3.1.3.6 Evaluation and Comparison of the Concepts; 3.1.4 Variation of Mission and Mach Numbers; 3.1.4.1 Mission Comparison; 3.1.4.2 Comparison of Mach Number Variation; 3.1.4.3 Accelerator Vehicle Concepts; 3.1.5 Trade Studies; 3.1.5.1 Airbreathing Second Stage; 3.1.5.2 LOX-Collection; 3.1.6 Comparison and Evaluation 3.1.7 Conclusion and Outlook3.2 Evaluation and Multidisciplinary Optimization of Two-Stage-to-Orbit Space Planes with Different Lower-Stage Concepts; 3.2.1 Introduction; 3.2.2 Reference Configurations; 3.2.2.1 Concept Design and Mission Requirements; 3.2.2.2 Space Plane Configuration with Lifting Body Lower Stage; 3.2.2.3 Space Plane Configuration with Waverider Lower Stage; 3.2.2.4 Design and Optimization Parameters; 3.2.3 Analysis Methods; 3.2.3.1 Quality Criteria; 3.2.3.2 Simulation and Optimization Software; 3.2.4 Performance of Reference Space Planes; 3.2.4.1 Mass Breakdown 3.2.4.2 Design Sensitivities3.2.5 Optimization Results; 3.2.5.1 Nominal Optimizations; 3.2.5.2 Sensitivity-Based Optimizations; 3.2.6 Summary and Conclusions; 4 Aerodynamics and Thermodynamics; 4.1 Low-Speed Tests with an ELAC-Model at High Reynolds Numbers; 4.1.1 Introduction; 4.1.2 Wind Tunnel Models; 4.1.3 Pressure Distributions Influenced by Reynolds Number; 4.1.4 Flow Field Influenced by Reynolds Number; 4.1.5 Force Coefficients Influenced by Reynolds Number; 4.1.6 Conclusion; 4.2 Experimental and Numerical Analysis of Supersonic Flow over the ELAC-Configuration; 4.2.1 Introduction 4.2.2 Experimental Setup4.2.3 Numerical Method; 4.2.4 Results; 4.2.4.1 Flow Over the Orbital Stage and the EOS/Flat Plate Configuration; 4.2.4.2 Separation of ELAC1C and EOS; 4.2.5 Conclusions; 4.3 Stage Separation - Aerodynamics and Flow Physics; 4.3.1 Introduction; 4.3.2 Methodology and Vehicle Geometries; 4.3.3 Numerical Simulation; 4.3.3.1 Flow Solver; 4.3.3.2 Grid Generation; 4.3.4 Experimental Simulation; 4.3.4.1 Models and Facility; 4.3.4.2 Measurement Technique and Test Programme; 4.3.5 Steady State Flow; 4.3.5.1 Dominant Flow Phenomena; 4.3.5.1.1 Inviscid Case - 2D and 3D Simulations 4.3.5.1.2 Viscous Effects - Laminar and Turbulent Flow |
| Record Nr. | UNINA-9910144586203321 |
| Weinheim, : Wiley-VCH, c2005 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Basic research and technologies for two-state-to-orbit vehicles [[electronic resource] ] : final report of the collaborative research centres / / edited by Dieter Jacob, Gottfried Sachs and Siegfried Wagner
| Basic research and technologies for two-state-to-orbit vehicles [[electronic resource] ] : final report of the collaborative research centres / / edited by Dieter Jacob, Gottfried Sachs and Siegfried Wagner |
| Pubbl/distr/stampa | Weinheim, : Wiley-VCH, c2005 |
| Descrizione fisica | 1 online resource (686 p.) |
| Disciplina |
629.4
629.47 |
| Altri autori (Persone) |
JacobDieter <1941->
SachsG (Gottfried) WagnerS <1937-2018.> (Siegfried) |
| Collana | Deutsche Forschung |
| Soggetto topico |
Space vehicles - Aerodynamics
Space vehicles - Design and construction Space vehicles - Materials Space vehicles - Thermodynamics |
| ISBN |
1-280-52056-6
9786610520565 3-527-60571-1 3-527-60550-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Basic Research and Technologies for Two-Stage-to-Orbit Vehicles; Contents; 1 Introduction; 2 Network Organization of Collaborative Research Centres for Scientific Efficiency Enhancement; 2.1 Introduction; 2.2 Organization of Collaboration; 2.3 Efficiency Enhancement in Research; 2.4 Efficiency Enhancement in Teaching and Education; 2.5 Internationalization; 2.6 Final Remarks; 3 Overall Design Aspects; 3.1 Conceptual Design of Winged Reusable Two-Stage-to-Orbit Space Transport Systems; 3.1.1 Background and Introduction; 3.1.2 Concepts for Reusable Space Transports
3.1.2.1 Single-Stage-to-Orbit SSTO3.1.2.2 Two-Stage-to-Orbit TSTO; 3.1.3 Design Procedure; 3.1.3.1 Design Tools and Methods; 3.1.3.2 Baseline Concept; 3.1.3.3 Boundary Conditions and Requirements; 3.1.3.4 Variation of Mission and Staging Mach Number; 3.1.3.5 Trade Studies; 3.1.3.6 Evaluation and Comparison of the Concepts; 3.1.4 Variation of Mission and Mach Numbers; 3.1.4.1 Mission Comparison; 3.1.4.2 Comparison of Mach Number Variation; 3.1.4.3 Accelerator Vehicle Concepts; 3.1.5 Trade Studies; 3.1.5.1 Airbreathing Second Stage; 3.1.5.2 LOX-Collection; 3.1.6 Comparison and Evaluation 3.1.7 Conclusion and Outlook3.2 Evaluation and Multidisciplinary Optimization of Two-Stage-to-Orbit Space Planes with Different Lower-Stage Concepts; 3.2.1 Introduction; 3.2.2 Reference Configurations; 3.2.2.1 Concept Design and Mission Requirements; 3.2.2.2 Space Plane Configuration with Lifting Body Lower Stage; 3.2.2.3 Space Plane Configuration with Waverider Lower Stage; 3.2.2.4 Design and Optimization Parameters; 3.2.3 Analysis Methods; 3.2.3.1 Quality Criteria; 3.2.3.2 Simulation and Optimization Software; 3.2.4 Performance of Reference Space Planes; 3.2.4.1 Mass Breakdown 3.2.4.2 Design Sensitivities3.2.5 Optimization Results; 3.2.5.1 Nominal Optimizations; 3.2.5.2 Sensitivity-Based Optimizations; 3.2.6 Summary and Conclusions; 4 Aerodynamics and Thermodynamics; 4.1 Low-Speed Tests with an ELAC-Model at High Reynolds Numbers; 4.1.1 Introduction; 4.1.2 Wind Tunnel Models; 4.1.3 Pressure Distributions Influenced by Reynolds Number; 4.1.4 Flow Field Influenced by Reynolds Number; 4.1.5 Force Coefficients Influenced by Reynolds Number; 4.1.6 Conclusion; 4.2 Experimental and Numerical Analysis of Supersonic Flow over the ELAC-Configuration; 4.2.1 Introduction 4.2.2 Experimental Setup4.2.3 Numerical Method; 4.2.4 Results; 4.2.4.1 Flow Over the Orbital Stage and the EOS/Flat Plate Configuration; 4.2.4.2 Separation of ELAC1C and EOS; 4.2.5 Conclusions; 4.3 Stage Separation - Aerodynamics and Flow Physics; 4.3.1 Introduction; 4.3.2 Methodology and Vehicle Geometries; 4.3.3 Numerical Simulation; 4.3.3.1 Flow Solver; 4.3.3.2 Grid Generation; 4.3.4 Experimental Simulation; 4.3.4.1 Models and Facility; 4.3.4.2 Measurement Technique and Test Programme; 4.3.5 Steady State Flow; 4.3.5.1 Dominant Flow Phenomena; 4.3.5.1.1 Inviscid Case - 2D and 3D Simulations 4.3.5.1.2 Viscous Effects - Laminar and Turbulent Flow |
| Record Nr. | UNINA-9910830287803321 |
| Weinheim, : Wiley-VCH, c2005 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Basic research and technologies for two-state-to-orbit vehicles [[electronic resource] ] : final report of the collaborative research centres / / edited by Dieter Jacob, Gottfried Sachs and Siegfried Wagner
| Basic research and technologies for two-state-to-orbit vehicles [[electronic resource] ] : final report of the collaborative research centres / / edited by Dieter Jacob, Gottfried Sachs and Siegfried Wagner |
| Pubbl/distr/stampa | Weinheim, : Wiley-VCH, c2005 |
| Descrizione fisica | 1 online resource (686 p.) |
| Disciplina |
629.4
629.47 |
| Altri autori (Persone) |
JacobDieter <1941->
SachsG (Gottfried) WagnerS <1937-2018.> (Siegfried) |
| Collana | Deutsche Forschung |
| Soggetto topico |
Space vehicles - Aerodynamics
Space vehicles - Design and construction Space vehicles - Materials Space vehicles - Thermodynamics |
| ISBN |
1-280-52056-6
9786610520565 3-527-60571-1 3-527-60550-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Basic Research and Technologies for Two-Stage-to-Orbit Vehicles; Contents; 1 Introduction; 2 Network Organization of Collaborative Research Centres for Scientific Efficiency Enhancement; 2.1 Introduction; 2.2 Organization of Collaboration; 2.3 Efficiency Enhancement in Research; 2.4 Efficiency Enhancement in Teaching and Education; 2.5 Internationalization; 2.6 Final Remarks; 3 Overall Design Aspects; 3.1 Conceptual Design of Winged Reusable Two-Stage-to-Orbit Space Transport Systems; 3.1.1 Background and Introduction; 3.1.2 Concepts for Reusable Space Transports
3.1.2.1 Single-Stage-to-Orbit SSTO3.1.2.2 Two-Stage-to-Orbit TSTO; 3.1.3 Design Procedure; 3.1.3.1 Design Tools and Methods; 3.1.3.2 Baseline Concept; 3.1.3.3 Boundary Conditions and Requirements; 3.1.3.4 Variation of Mission and Staging Mach Number; 3.1.3.5 Trade Studies; 3.1.3.6 Evaluation and Comparison of the Concepts; 3.1.4 Variation of Mission and Mach Numbers; 3.1.4.1 Mission Comparison; 3.1.4.2 Comparison of Mach Number Variation; 3.1.4.3 Accelerator Vehicle Concepts; 3.1.5 Trade Studies; 3.1.5.1 Airbreathing Second Stage; 3.1.5.2 LOX-Collection; 3.1.6 Comparison and Evaluation 3.1.7 Conclusion and Outlook3.2 Evaluation and Multidisciplinary Optimization of Two-Stage-to-Orbit Space Planes with Different Lower-Stage Concepts; 3.2.1 Introduction; 3.2.2 Reference Configurations; 3.2.2.1 Concept Design and Mission Requirements; 3.2.2.2 Space Plane Configuration with Lifting Body Lower Stage; 3.2.2.3 Space Plane Configuration with Waverider Lower Stage; 3.2.2.4 Design and Optimization Parameters; 3.2.3 Analysis Methods; 3.2.3.1 Quality Criteria; 3.2.3.2 Simulation and Optimization Software; 3.2.4 Performance of Reference Space Planes; 3.2.4.1 Mass Breakdown 3.2.4.2 Design Sensitivities3.2.5 Optimization Results; 3.2.5.1 Nominal Optimizations; 3.2.5.2 Sensitivity-Based Optimizations; 3.2.6 Summary and Conclusions; 4 Aerodynamics and Thermodynamics; 4.1 Low-Speed Tests with an ELAC-Model at High Reynolds Numbers; 4.1.1 Introduction; 4.1.2 Wind Tunnel Models; 4.1.3 Pressure Distributions Influenced by Reynolds Number; 4.1.4 Flow Field Influenced by Reynolds Number; 4.1.5 Force Coefficients Influenced by Reynolds Number; 4.1.6 Conclusion; 4.2 Experimental and Numerical Analysis of Supersonic Flow over the ELAC-Configuration; 4.2.1 Introduction 4.2.2 Experimental Setup4.2.3 Numerical Method; 4.2.4 Results; 4.2.4.1 Flow Over the Orbital Stage and the EOS/Flat Plate Configuration; 4.2.4.2 Separation of ELAC1C and EOS; 4.2.5 Conclusions; 4.3 Stage Separation - Aerodynamics and Flow Physics; 4.3.1 Introduction; 4.3.2 Methodology and Vehicle Geometries; 4.3.3 Numerical Simulation; 4.3.3.1 Flow Solver; 4.3.3.2 Grid Generation; 4.3.4 Experimental Simulation; 4.3.4.1 Models and Facility; 4.3.4.2 Measurement Technique and Test Programme; 4.3.5 Steady State Flow; 4.3.5.1 Dominant Flow Phenomena; 4.3.5.1.1 Inviscid Case - 2D and 3D Simulations 4.3.5.1.2 Viscous Effects - Laminar and Turbulent Flow |
| Record Nr. | UNINA-9910841548503321 |
| Weinheim, : Wiley-VCH, c2005 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
The design and uncertainty analysis of an improved total hemispherical emittance transient calorimeter / / by William R. Wade and Donald J. Progar
| The design and uncertainty analysis of an improved total hemispherical emittance transient calorimeter / / by William R. Wade and Donald J. Progar |
| Autore | Wade William R. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , March 1969 |
| Descrizione fisica | 1 online resource (20 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
Emissivity - Measurement - Equipment and supplies
Space vehicles - Materials - Thermal properties Space vehicles - Thermodynamics Heat - Transmission |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713905803321 |
Wade William R.
|
||
| Washington, D.C. : , : National Aeronautics and Space Administration, , March 1969 | ||
| Materiale a stampa | ||
| 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
| 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 | ||
| Materiale a stampa | ||
| 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
| 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 | ||
| Materiale a stampa | ||
| 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
| 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-9910816394303321 |
| New York, N.Y., : American Institute of Aeronautics and Astronautics, c1983 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
