Advances in energy and combustion : safety and sustainability / / A. K. Gupta [and four others], editors |
Edizione | [1st ed. 2022.] |
Pubbl/distr/stampa | Singapore : , : Springer, , [2021] |
Descrizione fisica | 1 online resource (XV, 600 p. 400 illus., 290 illus. in color.) |
Disciplina | 629.134353 |
Collana | Green Energy and Technology |
Soggetto topico |
Propulsion systems
Renewable energy sources - Research |
ISBN |
981-16-2647-2
981-16-2648-0 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Injector Dynamics and Pressure Gain in Rotating Detonation Engines -- Low Emissions Propulsion Engine Characterization Process -- Aerodynamic and Aero-Acoustic Performance of an Adjustable Pitch Axial Flow Fan -- Proposed Thrust Profile Design of Pulse Detonation Engine (PDE) for Aerospace Applications -- The Formation of PAH Compounds from the Combustion of Biofuels -- Review of Biomass Energy Resources with Livestock Manure -- Higher Alcohols as Diesel Engine Fuel -- Photocatalytic Hydrogen from Water over Semiconductors -- Evaluation of Hazard Correlations for Hydrogen Rich Fuels using Stretched Transient Flames -- Experimental Investigation of Turbulent Flow/Flame Structure of Double Swirler Burner. |
Record Nr. | UNINA-9910743265303321 |
Singapore : , : Springer, , [2021] | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Aircraft engine design / Jack D. Mattingly, William H. Heiser, Daniel H. Daley |
Autore | Mattingly, Jack D. |
Pubbl/distr/stampa | New York : American Institute of Aeronautics and Astronautics, 1987 |
Descrizione fisica | XXX, 582 p. : ill. ; 23 cm |
Disciplina | 629.134353 |
Altri autori (Persone) |
Heiser, William H.
Daley, Daniel H. |
Collana | AIAA Education series |
ISBN | 0-930403-23-1 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNINA-990008766400403321 |
Mattingly, Jack D. | ||
New York : American Institute of Aeronautics and Astronautics, 1987 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Aircraft propulsion and gas turbine engines / / Ahmed F. El-Sayed |
Autore | El-Sayed Ahmed F |
Edizione | [2nd ed.] |
Pubbl/distr/stampa | Boca Raton, Fla., : CRC P., 2017 |
Descrizione fisica | 1 online resource (xxvii, 1447 p.) : ill |
Disciplina | 629.134353 |
Soggetto topico |
Airplanes - Turbojet engines
Aircraft gas-turbines |
ISBN |
9781315156743 (e-book)
9781466595163 (hbk.) 1-4665-9518-3 1-315-15674-1 1-5231-1396-0 1-4665-9517-5 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Section I Aero engines and gas turbines -- 1. History and classifications of aero-engine -- 2. Performance parameters of jet engines -- 3. Pulsejet and ramjet engines -- 4. Turbojet engine -- 5. Turbofan engines -- 6. Shaft engines: internal combustion, turboprop, turboshaft, and propfan engines -- 7. High speed supersonic and hypersonic engines -- 8. Industrial gas turbines -- Section II Component design -- 9. Powerplant installation and intakes -- 10. Combustion systems -- 11. Exhaust system -- 12. Centrifugal compressors -- 13. Axial flow compressors and fans -- 14. Axial turbines -- 15. Radial inflow turbines -- 16. Module matching -- 17. Selected topics -- Section III Rocket propulsion -- 18. Introduction to rocketry -- 19. Rocket engines -- Appendix A: Glossary -- Appendix B: Turbofan -- Appendix C: Samples of gas turbines (representative manufacturers) -- Index. |
Record Nr. | UNINA-9910793188103321 |
El-Sayed Ahmed F | ||
Boca Raton, Fla., : CRC P., 2017 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Aircraft propulsion and gas turbine engines / / Ahmed F. El-Sayed |
Autore | El-Sayed Ahmed F |
Edizione | [2nd ed.] |
Pubbl/distr/stampa | Boca Raton, Fla., : CRC P., 2017 |
Descrizione fisica | 1 online resource (xxvii, 1447 p.) : ill |
Disciplina | 629.134353 |
Soggetto topico |
Airplanes - Turbojet engines
Aircraft gas-turbines |
ISBN |
9781315156743 (e-book)
9781466595163 (hbk.) 1-4665-9518-3 1-315-15674-1 1-5231-1396-0 1-4665-9517-5 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Section I Aero engines and gas turbines -- 1. History and classifications of aero-engine -- 2. Performance parameters of jet engines -- 3. Pulsejet and ramjet engines -- 4. Turbojet engine -- 5. Turbofan engines -- 6. Shaft engines: internal combustion, turboprop, turboshaft, and propfan engines -- 7. High speed supersonic and hypersonic engines -- 8. Industrial gas turbines -- Section II Component design -- 9. Powerplant installation and intakes -- 10. Combustion systems -- 11. Exhaust system -- 12. Centrifugal compressors -- 13. Axial flow compressors and fans -- 14. Axial turbines -- 15. Radial inflow turbines -- 16. Module matching -- 17. Selected topics -- Section III Rocket propulsion -- 18. Introduction to rocketry -- 19. Rocket engines -- Appendix A: Glossary -- Appendix B: Turbofan -- Appendix C: Samples of gas turbines (representative manufacturers) -- Index. |
Record Nr. | UNINA-9910806132403321 |
El-Sayed Ahmed F | ||
Boca Raton, Fla., : CRC P., 2017 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Filmkuhlung transsonischer Turbinen : Infrarotthermographisches Messverfahren zur Charakterisierung des Warmeubergangs / / Marco Ochs |
Autore | Ochs Marco |
Pubbl/distr/stampa | Berlin : , : Logos, , 2011 |
Descrizione fisica | 1 online resource (vi, 146 pages) : illustrations |
Disciplina | 629.134353 |
Soggetto topico |
Aircraft gas-turbines
Heat - Transmission |
Soggetto genere / forma | Electronic books. |
ISBN | 3-8325-9761-1 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | ger |
Record Nr. | UNINA-9910467449703321 |
Ochs Marco | ||
Berlin : , : Logos, , 2011 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Filmkuhlung transsonischer Turbinen : Infrarotthermographisches Messverfahren zur Charakterisierung des Warmeubergangs / / Marco Ochs |
Autore | Ochs Marco |
Pubbl/distr/stampa | Berlin : , : Logos, , 2011 |
Descrizione fisica | 1 online resource (vi, 146 pages) : illustrations |
Disciplina | 629.134353 |
Collana | Forschungsberichte aus dem Institut für Thermische Strömungsmaschinen |
Soggetto topico |
Aircraft gas-turbines
Heat - Transmission |
ISBN | 3-8325-9761-1 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | ger |
Record Nr. | UNINA-9910795210103321 |
Ochs Marco | ||
Berlin : , : Logos, , 2011 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Filmkuhlung transsonischer Turbinen : Infrarotthermographisches Messverfahren zur Charakterisierung des Warmeubergangs / / Marco Ochs |
Autore | Ochs Marco |
Pubbl/distr/stampa | Berlin : , : Logos, , 2011 |
Descrizione fisica | 1 online resource (vi, 146 pages) : illustrations |
Disciplina | 629.134353 |
Collana | Forschungsberichte aus dem Institut für Thermische Strömungsmaschinen |
Soggetto topico |
Aircraft gas-turbines
Heat - Transmission |
ISBN | 3-8325-9761-1 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | ger |
Record Nr. | UNINA-9910822604203321 |
Ochs Marco | ||
Berlin : , : Logos, , 2011 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Gas turbine propulsion systems |
Autore | MacIsaac Bernie |
Edizione | [2nd ed.] |
Pubbl/distr/stampa | Chicester : , : Wiley, , 2011 |
Descrizione fisica | 1 online resource (350 p.) |
Disciplina |
629.134/353
629.134353 |
Altri autori (Persone) | LangtonRoy |
Collana |
Aerospace series
THEi Wiley ebooks |
Soggetto topico |
Aircraft gas-turbines
Airplanes -- Turbojet engines Jet boat engines SCIENCE / System Theory Vehicles, Military Aircraft gas-turbines - Turbojet engines Airplanes Mechanical Engineering Engineering & Applied Sciences Aeronautics Engineering & Astronautics Mechanical Engineering - General |
ISBN |
1-283-20448-7
9786613204486 1-119-97548-4 1-119-97549-2 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
GAS TURBINE PROPULSION SYSTEMS; Contents; About the Authors; Preface; Series Preface; Acknowledgements; List of Acronyms; 1 Introduction; 1.1 Gas Turbine Concepts; 1.2 Gas Turbine Systems Overview; References; 2 Basic Gas Turbine Operation; 2.1 Turbojet Engine Performance; 2.1.1 Engine Performance Characteristics; 2.1.2 Compressor Surge Control; 2.1.3 Variable Nozzles; 2.2 Concluding Commentary; References; 3 Gas Generator Fuel Control Systems; 3.1 Basic Concepts of the Gas Generator Fuel Control System; 3.2 Gas Generator Control Modes; 3.2.1 Fuel Schedule Definition
3.2.2 Overall Gas Generator Control Logic3.2.3 Speed Governing with Acceleration and Deceleration Limiting; 3.2.4 Compressor Geometry Control; 3.2.5 Turbine Gas Temperature Limiting; 3.2.6 Overspeed Limiting; 3.3 Fuel System Design and Implementation; 3.3.1 A Historical Review of Fuel Control Technologies; 3.3.2 Fuel Pumping and Metering Systems; 3.4 The Concept of Error Budgets in Control Design; 3.4.1 Measurement Uncertainty; 3.4.2 Sources of Error; 3.5 Installation, Qualification, and Certification Considerations; 3.5.1 Fuel Handling Equipment 3.5.2 Full-authority Digital Engine Controls (FADEC)3.6 Concluding Commentary; References; 4 Thrust Engine Control and Augmentation Systems; 4.1 Thrust Engine Concepts; 4.2 Thrust Management and Control; 4.3 Thrust Augmentation; 4.3.1 Water Injection; 4.3.2 Afterburning; Reference; 5 Shaft Power Propulsion Control Systems; 5.1 Turboprop Applications; 5.1.1 The Single-shaft Engine; 5.1.2 The Free Turbine Turboprop; 5.2 Turboshaft Engine Applications; Reference; 6 Engine Inlet, Exhaust, and Nacelle Systems; 6.1 Subsonic Engine Air Inlets; 6.1.1 Basic Principles 6.1.2 Turboprop Inlet Configurations6.1.3 Inlet Filtration Systems; 6.2 Supersonic Engine Air Inlets; 6.2.1 Oblique Shockwaves; 6.2.2 Combined Oblique/Normal Shock Pressure Recovery Systems; 6.2.3 Supersonic Inlet Control; 6.2.4 Overall System Development and Operation; 6.2.5 Concorde Air Inlet Control System (AICS) Example; 6.3 Inlet Anti-icing; 6.3.1 Bleed-air Anti-icing Systems; 6.3.2 Electrical Anti-icing Systems; 6.4 Exhaust Systems; 6.4.1 Thrust Reversing Systems; 6.4.2 Thrust Vectoring Concepts; References; 7 Lubrication Systems; 7.1 Basic Principles; 7.2 Lubrication System Operation 7.2.1 System Design Concept7.2.2 System Design Considerations; 7.2.3 System Monitoring; 7.2.4 Ceramic Bearings; References; 8 Power Extraction and Starting Systems; 8.1 Mechanical Power Extraction; 8.1.1 Fuel Control Systems Equipment; 8.1.2 Hydraulic Power Extraction; 8.1.3 Lubrication and Scavenge Pumps; 8.1.4 Electrical Power Generation; 8.2 Engine Starting; 8.3 Bleed-air-powered Systems and Equipment; 8.3.1 Bleed-air-driven Pumps; 8.3.2 Bleed Air for Environmental Control, Pressurization and Anti-icing Systems; 8.3.3 Fuel Tank Inerting; References; 9 Marine Propulsion Systems 9.1 Propulsion System Designation |
Record Nr. | UNINA-9910133221503321 |
MacIsaac Bernie | ||
Chicester : , : Wiley, , 2011 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
High power laser propulsion / / Yuri A. Rezunkov |
Autore | Rezunkov Yuri A. |
Pubbl/distr/stampa | Cham, Switzerland : , : Springer, , [2021] |
Descrizione fisica | 1 online resource (307 pages) |
Disciplina | 629.134353 |
Collana | Springer Series on Atomic, Optical, and Plasma Physics |
Soggetto topico |
Propulsion systems
Lasers in astronautics |
ISBN | 3-030-79693-0 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
Intro -- Preface -- Acknowledgments -- Contents -- About the Author -- Abbreviations -- Chapter 1: A Brief History of Laser Propulsion -- 1.1 Introduction -- 1.2 Main Stages of Laser-Propulsion Developments -- 1.3 Physical Processes Underlying Laser Propulsion -- 1.3.1 General Classification of the Laser-Propulsion Phenomena -- 1.3.2 Basic Thrust Characteristics of Laser-Propulsion Engines -- 1.4 General Concepts of Laser Propulsion -- 1.4.1 Launching Space Vehicles into Low Earth Orbits with Laser Propulsion -- 1.4.2 Laser Propulsion for the Correction of LEO Satellites -- 1.4.3 Interorbital Missions of Space Vehicles with the Laser Propulsion -- 1.5 Original Concepts of High-Power Laser Propulsion -- 1.5.1 The ``4P´´ Vehicles -- 1.5.2 Lightcraft Technology Demonstrator (LTD) -- 1.5.3 Laser Impulse Space Propulsion-LISP -- 1.5.4 Principal Concept Design of the High-power Laser-Propulsion Systems -- References -- Chapter 2: Basic Gas-Dynamic Theories of the Laser Air-Breathing and Rocket Propulsion -- 2.1 Introduction -- 2.2 Gas-dynamic Theory of Laser Propulsion -- 2.2.1 Specific Properties of Pulsejet Laser Propulsion -- 2.2.2 Rocket Laser Propulsion at Space Conditions -- 2.2.2.1 Choice of a Propellant for Space Laser Propulsion -- 2.2.2.2 Determination of the Jet Nozzle Designs -- 2.3 Physics of Laser Plasma Ignited in Gases as Applied to Laser Propulsion -- 2.3.1 Model of Multi-Ionized Plasma Ignited by Laser Pulses in Gases -- 2.3.2 Conversion Efficiency of Laser Power into Plasma Temperature -- 2.4 Numerical Calculations of Non-stationary and Non-isentropic Gas Flows as Applied to Laser Propulsion -- 2.4.1 Perfect Gas Flow Models and Numerical Algorithms to Calculate Gas Flow of Pulsejet Laser Propulsion -- 2.4.2 Model of Equilibrium (Thermal) Plasma -- 2.4.3 Model of Non-equilibrium Plasma as Applied to Pulsejet Laser Propulsion.
2.4.4 Discussion on the Applicability of Various Models of Plasma Ignited -- References -- Chapter 3: Laser Ablation of Solid Materials, Laser Ablation Propulsion -- 3.1 Introduction -- 3.2 Physical Phenomena Underlying of Laser Ablation Propulsion -- 3.2.1 Basic Concept of Developed Evaporation of High-Melting and Low-Melting Materials -- 3.2.2 Simplified Gas-Dynamics Model of Laser ablation Propulsion -- 3.2.3 ``Absorption Explosion´´ Model of Plasma Ignition at Laser Ablation of Solid Targets -- 3.2.4 Gas-Dynamic Models of the Laser Radiation Interaction with Ionized Gas (Gaseous Plasma) -- 3.3 Effects of Solid Target Structure on Laser Ablation Propulsion -- 3.3.1 Direct Laser Ablation Propulsion -- 3.3.2 Combined Laser Ablation Propulsion -- 3.3.3 Confined Laser Ablation of Multilayer Structured Targets -- 3.4 Laser Ablation Propulsion Based on Ablation of High-Energy Polymers -- 3.4.1 Basic Plasma-chemical Reactions Proceeding in the CHO-Polymer Vapor Under Laser Radiation -- 3.4.2 Similarity Laws of Laser Ablation Propulsion Based on Polymer Propellants -- 3.5 Semi-empirical Models of Laser ablation Propulsion Based on CHO-Polymers -- 3.5.1 Gas-Dynamics of the Laser Ablation Propulsion -- 3.5.2 Vapor and Plasma Models of the Laser ablation Propulsion Using Critical Laser Power Flux -- 3.6 Efficiency of the Laser Ablation Propulsion Based on CHO-Polymers -- References -- Chapter 4: Aerospace Laser-Propulsion Engine -- 4.1 Introduction -- 4.2 The Aerospace Laser-Propulsion Engine Conception -- 4.2.1 Designing of Two-Mirror Beam Concentrator -- 4.2.2 Optical Model of the Two-Mirror Beam Concentrator -- 4.2.3 Numerical Techniques to Develop the Two-Mirror Beam Concentrator -- 4.3 ASLPE Thrust Characteristics in a Pulsed Mode of Operation -- 4.4 Adaptation of ASLPE for Continuous Wave (CW) Laser Propulsion -- 4.4.1 Principles of CW Laser Propulsion. 4.4.2 CW ASLPE Thrust Characteristics -- 4.5 Analysis of Available Technologies as Applied to ASLPE Development and its Engineering Constraints -- 4.5.1 Effects of Slit on Thrust Production -- 4.5.2 Thermo-physical Model of the ASLPE Device -- 4.6 Preliminary Conclusion -- References -- Chapter 5: Supersonic Laser Propulsion -- 5.1 Introduction -- 5.2 Lightcraft Engineering Version Adapted to the Pulsejet Supersonic Laser Propulsion -- 5.2.1 Perspective Designs of the Lightcraft -- 5.2.2 Intermediate Conclusion -- 5.3 Physical Phenomena Going with Ramjet Supersonic Laser Propulsion -- 5.3.1 Gas-Dynamics Effects Induced by Lasers in a Supersonic Gas Flow -- 5.4 Merging of Individual Shock Waves into a Quasi-Stationary Integrated Shock Wave -- 5.5 Supersonic Laser Ablation Propulsion -- 5.5.1 The Effects of Gas Jet Injection into Supersonic Gas Flows -- 5.5.2 Theoretical Model of Supersonic Laser Ablation Propulsion -- 5.5.3 Thrust Characteristics of Supersonic Laser Ablation Propulsion -- 5.5.4 Peculiar Properties of Thrust Production at the Supersonic Laser Ablation Propulsion -- 5.6 Conclusion -- References -- Chapter 6: Space Mini-vehicles with Laser Propulsion -- 6.1 Introduction to the Problem -- 6.2 Scenario of the SMV Orbital Maneuvers -- 6.3 Space Debris Removal Out of Geosynchronous Earth Orbit (GEO) by Using Laser-Propelled Space Mini-vehicles -- 6.4 Onboard Laser-Propulsion System as Applied to SMV -- 6.4.1 Receiver Telescope -- 6.4.2 Optical Turret -- 6.4.3 Optical Switch -- 6.4.4 The Unit of Laser-Propulsion Engines -- 6.4.5 Requirements to Optical Elements of the Onboard Laser-Propulsion System -- 6.5 Brief Outcome -- References -- Chapter 7: Laser Power Transfer to Space Vehicles with Laser Propulsion -- 7.1 Introduction into the Problem. 7.2 Models of the Aerosols and Gases Attenuation, Absorption, and Scattering of Laser Radiation in the Upper Atmosphere -- 7.2.1 Models of the Atmospheric Aerosols and Gases -- 7.2.2 Nonlinear Effects Developed During Propagation of High-Power Laser Radiation in the Upper Atmosphere -- 7.3 Self-Empirical Models of the Upper Atmosphere Turbulence -- 7.4 Phase and Intensity Profiles of the Laser Beam That Passed Through a Turbulent Atmosphere -- 7.4.1 Tentative Conclusion -- 7.5 Basic Atmospheric Effects Limiting Delivery of the Airborne Laser Power to Space Vehicle -- 7.5.1 Scenario of Laser Power Delivery to a Space Vehicle -- 7.5.2 Turbulence Effects on a Laser Beam as Applied to High-Power Laser Propulsion -- 7.6 Adaptive Laser Systems for the High-Power Laser Propulsion -- 7.6.1 Statement of the Problem -- 7.6.2 Adaptive Optical Laser Circuits and Special Equipment -- 7.6.2.1 Beam Wave Front Analyzers (BWA) -- 7.6.2.2 Beam Wave Front Phase Correctors -- 7.6.3 Laser Adaptive Optical Systems as Applied to Beaming a Remote Target -- 7.6.3.1 Linear Adaptive Laser Systems -- 7.6.3.2 Nonlinear Adaptive System Based on the Interaction of Laser Radiations with a Nonlinear Optical Medium -- 7.6.4 Principal Outcomes -- References -- Conclusion -- Index. |
Record Nr. | UNINA-9910495191903321 |
Rezunkov Yuri A. | ||
Cham, Switzerland : , : Springer, , [2021] | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
High power laser propulsion / / Yuri A. Rezunkov |
Autore | Rezunkov Yuri A. |
Pubbl/distr/stampa | Cham, Switzerland : , : Springer, , [2021] |
Descrizione fisica | 1 online resource (307 pages) |
Disciplina | 629.134353 |
Collana | Springer Series on Atomic, Optical, and Plasma Physics |
Soggetto topico |
Propulsion systems
Lasers in astronautics |
ISBN | 3-030-79693-0 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
Intro -- Preface -- Acknowledgments -- Contents -- About the Author -- Abbreviations -- Chapter 1: A Brief History of Laser Propulsion -- 1.1 Introduction -- 1.2 Main Stages of Laser-Propulsion Developments -- 1.3 Physical Processes Underlying Laser Propulsion -- 1.3.1 General Classification of the Laser-Propulsion Phenomena -- 1.3.2 Basic Thrust Characteristics of Laser-Propulsion Engines -- 1.4 General Concepts of Laser Propulsion -- 1.4.1 Launching Space Vehicles into Low Earth Orbits with Laser Propulsion -- 1.4.2 Laser Propulsion for the Correction of LEO Satellites -- 1.4.3 Interorbital Missions of Space Vehicles with the Laser Propulsion -- 1.5 Original Concepts of High-Power Laser Propulsion -- 1.5.1 The ``4P´´ Vehicles -- 1.5.2 Lightcraft Technology Demonstrator (LTD) -- 1.5.3 Laser Impulse Space Propulsion-LISP -- 1.5.4 Principal Concept Design of the High-power Laser-Propulsion Systems -- References -- Chapter 2: Basic Gas-Dynamic Theories of the Laser Air-Breathing and Rocket Propulsion -- 2.1 Introduction -- 2.2 Gas-dynamic Theory of Laser Propulsion -- 2.2.1 Specific Properties of Pulsejet Laser Propulsion -- 2.2.2 Rocket Laser Propulsion at Space Conditions -- 2.2.2.1 Choice of a Propellant for Space Laser Propulsion -- 2.2.2.2 Determination of the Jet Nozzle Designs -- 2.3 Physics of Laser Plasma Ignited in Gases as Applied to Laser Propulsion -- 2.3.1 Model of Multi-Ionized Plasma Ignited by Laser Pulses in Gases -- 2.3.2 Conversion Efficiency of Laser Power into Plasma Temperature -- 2.4 Numerical Calculations of Non-stationary and Non-isentropic Gas Flows as Applied to Laser Propulsion -- 2.4.1 Perfect Gas Flow Models and Numerical Algorithms to Calculate Gas Flow of Pulsejet Laser Propulsion -- 2.4.2 Model of Equilibrium (Thermal) Plasma -- 2.4.3 Model of Non-equilibrium Plasma as Applied to Pulsejet Laser Propulsion.
2.4.4 Discussion on the Applicability of Various Models of Plasma Ignited -- References -- Chapter 3: Laser Ablation of Solid Materials, Laser Ablation Propulsion -- 3.1 Introduction -- 3.2 Physical Phenomena Underlying of Laser Ablation Propulsion -- 3.2.1 Basic Concept of Developed Evaporation of High-Melting and Low-Melting Materials -- 3.2.2 Simplified Gas-Dynamics Model of Laser ablation Propulsion -- 3.2.3 ``Absorption Explosion´´ Model of Plasma Ignition at Laser Ablation of Solid Targets -- 3.2.4 Gas-Dynamic Models of the Laser Radiation Interaction with Ionized Gas (Gaseous Plasma) -- 3.3 Effects of Solid Target Structure on Laser Ablation Propulsion -- 3.3.1 Direct Laser Ablation Propulsion -- 3.3.2 Combined Laser Ablation Propulsion -- 3.3.3 Confined Laser Ablation of Multilayer Structured Targets -- 3.4 Laser Ablation Propulsion Based on Ablation of High-Energy Polymers -- 3.4.1 Basic Plasma-chemical Reactions Proceeding in the CHO-Polymer Vapor Under Laser Radiation -- 3.4.2 Similarity Laws of Laser Ablation Propulsion Based on Polymer Propellants -- 3.5 Semi-empirical Models of Laser ablation Propulsion Based on CHO-Polymers -- 3.5.1 Gas-Dynamics of the Laser Ablation Propulsion -- 3.5.2 Vapor and Plasma Models of the Laser ablation Propulsion Using Critical Laser Power Flux -- 3.6 Efficiency of the Laser Ablation Propulsion Based on CHO-Polymers -- References -- Chapter 4: Aerospace Laser-Propulsion Engine -- 4.1 Introduction -- 4.2 The Aerospace Laser-Propulsion Engine Conception -- 4.2.1 Designing of Two-Mirror Beam Concentrator -- 4.2.2 Optical Model of the Two-Mirror Beam Concentrator -- 4.2.3 Numerical Techniques to Develop the Two-Mirror Beam Concentrator -- 4.3 ASLPE Thrust Characteristics in a Pulsed Mode of Operation -- 4.4 Adaptation of ASLPE for Continuous Wave (CW) Laser Propulsion -- 4.4.1 Principles of CW Laser Propulsion. 4.4.2 CW ASLPE Thrust Characteristics -- 4.5 Analysis of Available Technologies as Applied to ASLPE Development and its Engineering Constraints -- 4.5.1 Effects of Slit on Thrust Production -- 4.5.2 Thermo-physical Model of the ASLPE Device -- 4.6 Preliminary Conclusion -- References -- Chapter 5: Supersonic Laser Propulsion -- 5.1 Introduction -- 5.2 Lightcraft Engineering Version Adapted to the Pulsejet Supersonic Laser Propulsion -- 5.2.1 Perspective Designs of the Lightcraft -- 5.2.2 Intermediate Conclusion -- 5.3 Physical Phenomena Going with Ramjet Supersonic Laser Propulsion -- 5.3.1 Gas-Dynamics Effects Induced by Lasers in a Supersonic Gas Flow -- 5.4 Merging of Individual Shock Waves into a Quasi-Stationary Integrated Shock Wave -- 5.5 Supersonic Laser Ablation Propulsion -- 5.5.1 The Effects of Gas Jet Injection into Supersonic Gas Flows -- 5.5.2 Theoretical Model of Supersonic Laser Ablation Propulsion -- 5.5.3 Thrust Characteristics of Supersonic Laser Ablation Propulsion -- 5.5.4 Peculiar Properties of Thrust Production at the Supersonic Laser Ablation Propulsion -- 5.6 Conclusion -- References -- Chapter 6: Space Mini-vehicles with Laser Propulsion -- 6.1 Introduction to the Problem -- 6.2 Scenario of the SMV Orbital Maneuvers -- 6.3 Space Debris Removal Out of Geosynchronous Earth Orbit (GEO) by Using Laser-Propelled Space Mini-vehicles -- 6.4 Onboard Laser-Propulsion System as Applied to SMV -- 6.4.1 Receiver Telescope -- 6.4.2 Optical Turret -- 6.4.3 Optical Switch -- 6.4.4 The Unit of Laser-Propulsion Engines -- 6.4.5 Requirements to Optical Elements of the Onboard Laser-Propulsion System -- 6.5 Brief Outcome -- References -- Chapter 7: Laser Power Transfer to Space Vehicles with Laser Propulsion -- 7.1 Introduction into the Problem. 7.2 Models of the Aerosols and Gases Attenuation, Absorption, and Scattering of Laser Radiation in the Upper Atmosphere -- 7.2.1 Models of the Atmospheric Aerosols and Gases -- 7.2.2 Nonlinear Effects Developed During Propagation of High-Power Laser Radiation in the Upper Atmosphere -- 7.3 Self-Empirical Models of the Upper Atmosphere Turbulence -- 7.4 Phase and Intensity Profiles of the Laser Beam That Passed Through a Turbulent Atmosphere -- 7.4.1 Tentative Conclusion -- 7.5 Basic Atmospheric Effects Limiting Delivery of the Airborne Laser Power to Space Vehicle -- 7.5.1 Scenario of Laser Power Delivery to a Space Vehicle -- 7.5.2 Turbulence Effects on a Laser Beam as Applied to High-Power Laser Propulsion -- 7.6 Adaptive Laser Systems for the High-Power Laser Propulsion -- 7.6.1 Statement of the Problem -- 7.6.2 Adaptive Optical Laser Circuits and Special Equipment -- 7.6.2.1 Beam Wave Front Analyzers (BWA) -- 7.6.2.2 Beam Wave Front Phase Correctors -- 7.6.3 Laser Adaptive Optical Systems as Applied to Beaming a Remote Target -- 7.6.3.1 Linear Adaptive Laser Systems -- 7.6.3.2 Nonlinear Adaptive System Based on the Interaction of Laser Radiations with a Nonlinear Optical Medium -- 7.6.4 Principal Outcomes -- References -- Conclusion -- Index. |
Record Nr. | UNISA-996466739003316 |
Rezunkov Yuri A. | ||
Cham, Switzerland : , : Springer, , [2021] | ||
Materiale a stampa | ||
Lo trovi qui: Univ. di Salerno | ||
|