Assessment of options for extending the life of the Hubble Space Telescope [[electronic resource] ] : final report / / Committee on the Assessment of Options for Extending the Life of the Hubble Space Telescope, Space Studies Board, Aeronautics and Space Engineering Board, Division on Engineering and Physical Sciences, National Research Council of the National Academies ; [Louis J. Lanzerotti, chair] |
Pubbl/distr/stampa | Washington, D.C., : National Academies Press, 2005 |
Descrizione fisica | 1 online resource (161 p.) |
Disciplina | 629.44/1 |
Altri autori (Persone) | LanzerottiLouis J |
Soggetto genere / forma | Electronic books. |
ISBN |
1-283-37650-4
9786613376503 0-309-54745-8 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Front Matter""; ""Acknowledgment of Reviewers""; ""Contents""; ""Executive Summary""; ""1 Introduction""; ""2 Hubble Space Telescope""; ""3 The Impact of Hubble: Past and Future""; ""4 HST Observatory Assessment and Lifetime Projection""; ""5 HST Robotic Servicing Assessment""; ""6 Space Shuttle Servicing of Hubble""; ""7 Benefit/Risk Assessment of Hubble Space Telescope Servicing Options""; ""8 Conclusions and Recommendations""; ""Appendixes""; ""A Statement of Task""; ""B Briefings to the Committee""; ""C Interim Report""; ""D State of the Art in Robotics""; ""E Acronyms""; ""F Glossary""
""G Biographical Information for Committee Members and Staff"" |
Record Nr. | UNINA-9910457675603321 |
Washington, D.C., : National Academies Press, 2005 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Assessment of options for extending the life of the Hubble Space Telescope [[electronic resource] ] : final report / / Committee on the Assessment of Options for Extending the Life of the Hubble Space Telescope, Space Studies Board, Aeronautics and Space Engineering Board, Division on Engineering and Physical Sciences, National Research Council of the National Academies ; [Louis J. Lanzerotti, chair] |
Pubbl/distr/stampa | Washington, D.C., : National Academies Press, 2005 |
Descrizione fisica | 1 online resource (161 p.) |
Disciplina | 629.44/1 |
Altri autori (Persone) | LanzerottiLouis J |
ISBN |
0-309-16545-8
1-283-37650-4 9786613376503 0-309-54745-8 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Front Matter""; ""Acknowledgment of Reviewers""; ""Contents""; ""Executive Summary""; ""1 Introduction""; ""2 Hubble Space Telescope""; ""3 The Impact of Hubble: Past and Future""; ""4 HST Observatory Assessment and Lifetime Projection""; ""5 HST Robotic Servicing Assessment""; ""6 Space Shuttle Servicing of Hubble""; ""7 Benefit/Risk Assessment of Hubble Space Telescope Servicing Options""; ""8 Conclusions and Recommendations""; ""Appendixes""; ""A Statement of Task""; ""B Briefings to the Committee""; ""C Interim Report""; ""D State of the Art in Robotics""; ""E Acronyms""; ""F Glossary""
""G Biographical Information for Committee Members and Staff"" |
Record Nr. | UNINA-9910781610503321 |
Washington, D.C., : National Academies Press, 2005 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Assessment of options for extending the life of the Hubble Space Telescope : final report / / Committee on the Assessment of Options for Extending the Life of the Hubble Space Telescope, Space Studies Board, Aeronautics and Space Engineering Board, Division on Engineering and Physical Sciences, National Research Council of the National Academies ; [Louis J. Lanzerotti, chair] |
Edizione | [1st ed.] |
Pubbl/distr/stampa | Washington, D.C., : National Academies Press, 2005 |
Descrizione fisica | 1 online resource (161 p.) |
Disciplina | 629.44/1 |
Altri autori (Persone) | LanzerottiLouis J |
ISBN |
0-309-16545-8
1-283-37650-4 9786613376503 0-309-54745-8 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Front Matter""; ""Acknowledgment of Reviewers""; ""Contents""; ""Executive Summary""; ""1 Introduction""; ""2 Hubble Space Telescope""; ""3 The Impact of Hubble: Past and Future""; ""4 HST Observatory Assessment and Lifetime Projection""; ""5 HST Robotic Servicing Assessment""; ""6 Space Shuttle Servicing of Hubble""; ""7 Benefit/Risk Assessment of Hubble Space Telescope Servicing Options""; ""8 Conclusions and Recommendations""; ""Appendixes""; ""A Statement of Task""; ""B Briefings to the Committee""; ""C Interim Report""; ""D State of the Art in Robotics""; ""E Acronyms""; ""F Glossary""
""G Biographical Information for Committee Members and Staff"" |
Record Nr. | UNINA-9910826886903321 |
Washington, D.C., : National Academies Press, 2005 | ||
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 |
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 |
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 |
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 | ||
|
The space shuttle / / by Jeffrey Zuehlke |
Autore | Zuehlke Jeffrey <1968-> |
Pubbl/distr/stampa | Minneapolis : , : Learner Publications Company, , [2007] |
Descrizione fisica | 1 online resource (32 pages) : illustrations |
Disciplina | 629.44/1 |
Collana | Pull ahead books The space shuttle |
Soggetto topico | Space shuttles |
ISBN |
1-281-28264-2
9786611282646 0-8225-8954-0 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-9910693333403321 |
Zuehlke Jeffrey <1968-> | ||
Minneapolis : , : Learner Publications Company, , [2007] | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Thermal design of aeroassisted orbital transfer vehicles [[electronic resource] /] / edited by H.F. Nelson |
Pubbl/distr/stampa | New York, : American Institute of Aeronautics and Astronautics, c1985 |
Descrizione fisica | 1 online resource (573 p.) |
Disciplina |
629.1 s
629.44/1 |
Altri autori (Persone) | NelsonH. F |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Orbital transfer (Space flight)
Space vehicles - Thermodynamics Space vehicles - Atmospheric entry |
Soggetto genere / forma | Electronic books. |
ISBN |
1-60086-571-2
1-60086-352-3 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Editorial Committee""; ""Chapter I. Flowfield Analysis""; ""Basic Governing Equations for the Flight Regimes of Aeroassisted Orbital Transfer Vehicles""; ""Complete Flowfields Over Low- and Wide-Angle AOTV Conceptual Configurations""; ""AOTV Bluff Body Flow�Relaxation Algorithm""; ""Direct Simulation of Transitional Flow for Hypersonic Re-entry Conditions""; ""Chapter II. Trajectories""; ""Performance Evaluation of the Atmospheric Phase of Two Aeromaneuvering Orbital Transfer Vehicles""
""Performance Aerodynamics of Aeroassisted Orbital Transfer Vehicles""""Multiple Pass Trajectories for an Aeroassisted Orbital Transfer Vehicle""; ""Impact of Atmospheric Uncertainties and Viscous Interaction Effects on the Performance of Aeroassisted Orbital Transfer Vehicles""; ""Analytical Characterization of AOTV Perigee Aerothermodynamic Regime""; ""Chapter III. Thermal Protection""; ""Thermal Protection Requirements for Near-Earth Aeroassisted Orbital Transfer Vehicle Missions""; ""Design and Performance Analysis of a Conical Aerobrake Orbital Transfer Vehicle Concept"" ""An AOTV Aeroheating and Thermal Protection Study""""Aerothermodynamic Heating Analysis of Aerobraking and Aeromaneuvering Orbital Transfer Vehicles""; ""Thermal Response of an Aeroassisted Orbital Transfer Vehicle with a Conical Drag Brake""; ""Low Lift-to-Drag Aerobrake Heat-Transfer Test at Mach 10""; ""Calculation of Nonequilibrium Radiation in the Flight Regimes of Aeroassisted Orbital Transfer Vehicles""; ""Air Radiation Revisited""; ""Chapter IV. Surface Effects""; ""Temperature-Dependent Reaction Rate Expressions for Oxygen Recombination"" ""Surface-Slip Equations for Low Reynolds Number Multicomponent Air Flow""""Comparison of Viscous Shock-Layer Heating Analysis with Shuttle Flight Data in Slip Flow Regime""; ""Problems of Rate Chemistry in the Flight Regimes of Aeroassisted Orbital Transfer Vehicles""; ""Progress in Noncatalytic Surfaces for Metallic Heat Shields""; ""Author Index"" |
Record Nr. | UNINA-9910457201503321 |
New York, : American Institute of Aeronautics and Astronautics, c1985 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Thermal design of aeroassisted orbital transfer vehicles [[electronic resource] /] / edited by H.F. Nelson |
Pubbl/distr/stampa | New York, : American Institute of Aeronautics and Astronautics, c1985 |
Descrizione fisica | 1 online resource (573 p.) |
Disciplina |
629.1 s
629.44/1 |
Altri autori (Persone) | NelsonH. F |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Orbital transfer (Space flight)
Space vehicles - Thermodynamics Space vehicles - Atmospheric entry |
ISBN |
1-60086-571-2
1-60086-352-3 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Editorial Committee""; ""Chapter I. Flowfield Analysis""; ""Basic Governing Equations for the Flight Regimes of Aeroassisted Orbital Transfer Vehicles""; ""Complete Flowfields Over Low- and Wide-Angle AOTV Conceptual Configurations""; ""AOTV Bluff Body Flow�Relaxation Algorithm""; ""Direct Simulation of Transitional Flow for Hypersonic Re-entry Conditions""; ""Chapter II. Trajectories""; ""Performance Evaluation of the Atmospheric Phase of Two Aeromaneuvering Orbital Transfer Vehicles""
""Performance Aerodynamics of Aeroassisted Orbital Transfer Vehicles""""Multiple Pass Trajectories for an Aeroassisted Orbital Transfer Vehicle""; ""Impact of Atmospheric Uncertainties and Viscous Interaction Effects on the Performance of Aeroassisted Orbital Transfer Vehicles""; ""Analytical Characterization of AOTV Perigee Aerothermodynamic Regime""; ""Chapter III. Thermal Protection""; ""Thermal Protection Requirements for Near-Earth Aeroassisted Orbital Transfer Vehicle Missions""; ""Design and Performance Analysis of a Conical Aerobrake Orbital Transfer Vehicle Concept"" ""An AOTV Aeroheating and Thermal Protection Study""""Aerothermodynamic Heating Analysis of Aerobraking and Aeromaneuvering Orbital Transfer Vehicles""; ""Thermal Response of an Aeroassisted Orbital Transfer Vehicle with a Conical Drag Brake""; ""Low Lift-to-Drag Aerobrake Heat-Transfer Test at Mach 10""; ""Calculation of Nonequilibrium Radiation in the Flight Regimes of Aeroassisted Orbital Transfer Vehicles""; ""Air Radiation Revisited""; ""Chapter IV. Surface Effects""; ""Temperature-Dependent Reaction Rate Expressions for Oxygen Recombination"" ""Surface-Slip Equations for Low Reynolds Number Multicomponent Air Flow""""Comparison of Viscous Shock-Layer Heating Analysis with Shuttle Flight Data in Slip Flow Regime""; ""Problems of Rate Chemistry in the Flight Regimes of Aeroassisted Orbital Transfer Vehicles""; ""Progress in Noncatalytic Surfaces for Metallic Heat Shields""; ""Author Index"" |
Record Nr. | UNINA-9910781699803321 |
New York, : American Institute of Aeronautics and Astronautics, c1985 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Thermal design of aeroassisted orbital transfer vehicles [[electronic resource] /] / edited by H.F. Nelson |
Pubbl/distr/stampa | New York, : American Institute of Aeronautics and Astronautics, c1985 |
Descrizione fisica | 1 online resource (573 p.) |
Disciplina |
629.1 s
629.44/1 |
Altri autori (Persone) | NelsonH. F |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Orbital transfer (Space flight)
Space vehicles - Thermodynamics Space vehicles - Atmospheric entry |
ISBN |
1-60086-571-2
1-60086-352-3 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Editorial Committee""; ""Chapter I. Flowfield Analysis""; ""Basic Governing Equations for the Flight Regimes of Aeroassisted Orbital Transfer Vehicles""; ""Complete Flowfields Over Low- and Wide-Angle AOTV Conceptual Configurations""; ""AOTV Bluff Body Flow�Relaxation Algorithm""; ""Direct Simulation of Transitional Flow for Hypersonic Re-entry Conditions""; ""Chapter II. Trajectories""; ""Performance Evaluation of the Atmospheric Phase of Two Aeromaneuvering Orbital Transfer Vehicles""
""Performance Aerodynamics of Aeroassisted Orbital Transfer Vehicles""""Multiple Pass Trajectories for an Aeroassisted Orbital Transfer Vehicle""; ""Impact of Atmospheric Uncertainties and Viscous Interaction Effects on the Performance of Aeroassisted Orbital Transfer Vehicles""; ""Analytical Characterization of AOTV Perigee Aerothermodynamic Regime""; ""Chapter III. Thermal Protection""; ""Thermal Protection Requirements for Near-Earth Aeroassisted Orbital Transfer Vehicle Missions""; ""Design and Performance Analysis of a Conical Aerobrake Orbital Transfer Vehicle Concept"" ""An AOTV Aeroheating and Thermal Protection Study""""Aerothermodynamic Heating Analysis of Aerobraking and Aeromaneuvering Orbital Transfer Vehicles""; ""Thermal Response of an Aeroassisted Orbital Transfer Vehicle with a Conical Drag Brake""; ""Low Lift-to-Drag Aerobrake Heat-Transfer Test at Mach 10""; ""Calculation of Nonequilibrium Radiation in the Flight Regimes of Aeroassisted Orbital Transfer Vehicles""; ""Air Radiation Revisited""; ""Chapter IV. Surface Effects""; ""Temperature-Dependent Reaction Rate Expressions for Oxygen Recombination"" ""Surface-Slip Equations for Low Reynolds Number Multicomponent Air Flow""""Comparison of Viscous Shock-Layer Heating Analysis with Shuttle Flight Data in Slip Flow Regime""; ""Problems of Rate Chemistry in the Flight Regimes of Aeroassisted Orbital Transfer Vehicles""; ""Progress in Noncatalytic Surfaces for Metallic Heat Shields""; ""Author Index"" |
Record Nr. | UNINA-9910818945603321 |
New York, : American Institute of Aeronautics and Astronautics, c1985 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|