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Fusion energy in space propulsion [[electronic resource] /] / edited by Terry Kammash
| Fusion energy in space propulsion [[electronic resource] /] / edited by Terry Kammash |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, c1995 |
| Descrizione fisica | 1 online resource (263 p.) |
| Disciplina | 629.47/53 |
| Altri autori (Persone) | KammashTerry |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Nuclear fusion
Space vehicles - Propulsion systems |
| ISBN |
1-60086-635-2
1-60086-416-3 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Principles of Fusion Energy Utilization in Space Propulsion""; ""High-Performance Fusion Rocket for Manned Space Missions""; ""An Antiprotpon Catalyzed Inertial Fusion Propulsion System""; ""Comparison of Fusion/Antiproton Propulsion Systems for Interplanetary Travel""; ""An Antiproton Driver for Internal Confinement Fusion Propulsion""; ""From SSTO to Saturn's Moons: Superperformance Fusion Propulsion for Practical Spaceflight""
""Innovative Technology for an Inertial Electrostatic Confinement (IEC) Fusion Propulsion Unit""""Fusion Plasma Thruster Using a Dense Plasma Focus Device""; ""Performance of Fusion-Fission Hybrid Nuclear Rocket Engine""; ""Magnetic Control of Fission Plasmas""; ""The Outer Solar System and the Human Future""; ""Author Index"" |
| Record Nr. | UNINA-9910781401603321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, c1995 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Fusion energy in space propulsion [[electronic resource] /] / edited by Terry Kammash
| Fusion energy in space propulsion [[electronic resource] /] / edited by Terry Kammash |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, c1995 |
| Descrizione fisica | 1 online resource (263 p.) |
| Disciplina | 629.47/53 |
| Altri autori (Persone) | KammashTerry |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Nuclear fusion
Space vehicles - Propulsion systems |
| ISBN |
1-60086-635-2
1-60086-416-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Principles of Fusion Energy Utilization in Space Propulsion""; ""High-Performance Fusion Rocket for Manned Space Missions""; ""An Antiprotpon Catalyzed Inertial Fusion Propulsion System""; ""Comparison of Fusion/Antiproton Propulsion Systems for Interplanetary Travel""; ""An Antiproton Driver for Internal Confinement Fusion Propulsion""; ""From SSTO to Saturn's Moons: Superperformance Fusion Propulsion for Practical Spaceflight""
""Innovative Technology for an Inertial Electrostatic Confinement (IEC) Fusion Propulsion Unit""""Fusion Plasma Thruster Using a Dense Plasma Focus Device""; ""Performance of Fusion-Fission Hybrid Nuclear Rocket Engine""; ""Magnetic Control of Fission Plasmas""; ""The Outer Solar System and the Human Future""; ""Author Index"" |
| Record Nr. | UNINA-9910810023203321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, c1995 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Future spacecraft propulsion systems : enabling technologies for space exploration / Paul A. Czysz and Claudio Bruno
| Future spacecraft propulsion systems : enabling technologies for space exploration / Paul A. Czysz and Claudio Bruno |
| Autore | Czysz, Paul A. |
| Pubbl/distr/stampa | Berlin ; New York : Springer |
| Descrizione fisica | xxvi, 464 p. : ill. ; 25 cm |
| Disciplina | 629.475 |
| Altri autori (Persone) | Bruno, Claudioauthor |
| Collana | Springer-Praxis books in astronautical engineering |
| Soggetto topico | Space vehicles - Propulsion systems |
| ISBN | 3540231617 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNISALENTO-991001804949707536 |
Czysz, Paul A.
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| Berlin ; New York : Springer | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. del Salento | ||
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Future spacecraft propulsion systems and integration : enabling technologies for space exploration / / Paul A. Czysz, Claudio Bruno, Bernd Chudoba
| Future spacecraft propulsion systems and integration : enabling technologies for space exploration / / Paul A. Czysz, Claudio Bruno, Bernd Chudoba |
| Autore | Czysz Paul A |
| Edizione | [3rd edition 2018.] |
| Pubbl/distr/stampa | Berlin, Heidelberg : , : Springer Berlin Heidelberg : , : Imprint : Springer, , 2018 |
| Descrizione fisica | 1 online resource (LXI, 463 p.) : 349 illus |
| Disciplina | 629.1 |
| Collana | Astronautical Engineering |
| Soggetto topico |
Space vehicles - Propulsion systems
Aerospace Technology and Astronautics Space Sciences (including Extraterrestrial Physics, Space Exploration and Astronautics) |
| ISBN | 3-662-54744-9 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Overview -- Our progress appears to be impeded -- Commercial near-Earth space launcher: a perspective -- Commercial near-Earth launcher: propulsion -- Earth orbit on-orbit operations in near-Earth orbit, a necessary second step -- Earth-Moon system: establishing a Solar System presence -- Exploration of our Solar System -- Stellar and interstellar precursor missions -- View to the future and exploration of our Galaxy. |
| Record Nr. | UNINA-9910299572603321 |
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Czysz Paul A
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| Berlin, Heidelberg : , : Springer Berlin Heidelberg : , : Imprint : Springer, , 2018 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Ion beam characterization of a NEXT multi-thruster array plume [[electronic resource] /] / Eric J. Pencil ... [and others]
| Ion beam characterization of a NEXT multi-thruster array plume [[electronic resource] /] / Eric J. Pencil ... [and others] |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2006] |
| Descrizione fisica | 1 online resource (20 pages) : color illustrations |
| Altri autori (Persone) | PencilEric J |
| Collana | NASA/TM |
| Soggetto topico |
Space vehicles - Propulsion systems
Electric power systems |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697245603321 |
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2006] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Liquid acquisition devices for advanced in-space cryogenic propulsion systems / / Jason William Hartwig
| Liquid acquisition devices for advanced in-space cryogenic propulsion systems / / Jason William Hartwig |
| Autore | Hartwig Jason William |
| Pubbl/distr/stampa | London, England : , : Academic Press, , 2016 |
| Descrizione fisica | 1 online resource (489 p.) |
| Disciplina | 629.475 |
| Soggetto topico |
Space vehicles - Propulsion systems
Space vehicles - Electronic equipment |
| ISBN | 0-12-803990-6 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front Cover; Liquid Acquisition Devices for Advanced In-Space Cryogenic Propulsion Systems; Copyright; Dedication; Contents; Foreword; Preface; Acknowledgments; Chapter 1: Introduction; 1.1. The Flexible Path; 1.2. Fundamental Cryogenic Fluids; 1.3. Motivation for Cryogenic Propulsion Technology Development; 1.4. Existing Challenges with Cryogenic Propellants; 1.5. Cryogenic Fluid Management Subsystems; 1.6. Future Cryogenic Fluid Management Applications; 1.6.1. In-Space Cryogenic Engines; 1.6.2. In-Space Cryogenic Fuel Depots; 1.7. Purpose of Work and Overview by Chapter
Chapter 2: Background and Historical Review2.1. Propellant Management Device Purpose; 2.2. Other Types of Propellant Management Devices; 2.3. Vanes; 2.3.1. Design Concept, Basic Flow Physics, and Principle of Operation; 2.3.2. Advantages and Disadvantages; 2.3.3. Storable Propellant Historical Examples; 2.3.3.1. Space Experiments; 2.3.3.2. Vehicles and Missions; 2.4. Sponges; 2.4.1. Design Concept, Basic Flow Physics, and Principle of Operation; 2.4.2. Advantages and Disadvantages; 2.4.3. Storable Propellant Historical Examples; 2.4.3.1. Space Experiments; 2.4.3.2. Vehicles and Missions 2.5. Screen Channel Liquid Acquisition Devices2.5.1. Design Concept, Basic Flow Physics, and Principle of Operation; 2.5.2. Mesh and Metal Type; 2.5.3. Advantages and Disadvantages; 2.5.4. Storable Propellant Historical Examples; 2.5.4.1. Space Experiments; 2.5.4.2. Vehicles and Missions; 2.5.5. Cryogenic Propellant Historical Examples; 2.6. Propellant Management Device Combinations; 2.7. NASA's Current Needs; Chapter 3: Influential Factors and Physics-Based Modeling of Liquid Acquisition Devices; 3.1. 1-g One Dimensional Simplified Pressure Drop Model 3.2. The Room Temperature Bubble Point Pressure3.2.1. Assumptions; 3.2.2. Bubble Point Model Derivation; 3.2.3. Types of Bubble Point Experiments; 3.2.4. Surface Tension Model; 3.2.5. Specifying the Effective Pore Diameter; 3.2.6. Previously Reported Bubble Points; 3.3. Hydrostatic Pressure Drop; 3.4. Flow-Through-Screen Pressure Drop; 3.4.1. Model Derivation; 3.4.2. Model Parameters and Flow-Through-Screen Experiment; 3.4.3. Historical Data and Trends; 3.5. Frictional and Dynamic Pressure Drop; 3.6. Wicking Rate; 3.6.1. Model Derivation; 3.6.2. Wicking Rate Experiment 3.6.3. Historical Data and Trends3.7. Screen Compliance; 3.7.1. Model Derivation and Screen Compliance Experiment; 3.7.2. Historical Data and Trends; 3.8. Material Compatibility; 3.9. The Room Temperature Reseal Pressure Model; 3.9.1. Model Derivation; 3.9.2. Historical Data and Trends; 3.9.3. Specifying the Reseal Diameter; 3.10. Pressurant Gas Type; 3.11. Concluding Remarks and Implications for Cryogenic Propulsion Systems; Chapter 4: Room Temperature Liquid Acquisition Device Performance Experiments; 4.1. Pure Fluid Tests; 4.1.1. Scanning Electron Microscopy Analysis 4.1.2. Bubble Point Experimental Setup |
| Record Nr. | UNINA-9910797980003321 |
|
Hartwig Jason William
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| London, England : , : Academic Press, , 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Liquid acquisition devices for advanced in-space cryogenic propulsion systems / / Jason William Hartwig
| Liquid acquisition devices for advanced in-space cryogenic propulsion systems / / Jason William Hartwig |
| Autore | Hartwig Jason William |
| Pubbl/distr/stampa | London, England : , : Academic Press, , 2016 |
| Descrizione fisica | 1 online resource (489 p.) |
| Disciplina | 629.475 |
| Soggetto topico |
Space vehicles - Propulsion systems
Space vehicles - Electronic equipment |
| ISBN | 0-12-803990-6 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front Cover; Liquid Acquisition Devices for Advanced In-Space Cryogenic Propulsion Systems; Copyright; Dedication; Contents; Foreword; Preface; Acknowledgments; Chapter 1: Introduction; 1.1. The Flexible Path; 1.2. Fundamental Cryogenic Fluids; 1.3. Motivation for Cryogenic Propulsion Technology Development; 1.4. Existing Challenges with Cryogenic Propellants; 1.5. Cryogenic Fluid Management Subsystems; 1.6. Future Cryogenic Fluid Management Applications; 1.6.1. In-Space Cryogenic Engines; 1.6.2. In-Space Cryogenic Fuel Depots; 1.7. Purpose of Work and Overview by Chapter
Chapter 2: Background and Historical Review2.1. Propellant Management Device Purpose; 2.2. Other Types of Propellant Management Devices; 2.3. Vanes; 2.3.1. Design Concept, Basic Flow Physics, and Principle of Operation; 2.3.2. Advantages and Disadvantages; 2.3.3. Storable Propellant Historical Examples; 2.3.3.1. Space Experiments; 2.3.3.2. Vehicles and Missions; 2.4. Sponges; 2.4.1. Design Concept, Basic Flow Physics, and Principle of Operation; 2.4.2. Advantages and Disadvantages; 2.4.3. Storable Propellant Historical Examples; 2.4.3.1. Space Experiments; 2.4.3.2. Vehicles and Missions 2.5. Screen Channel Liquid Acquisition Devices2.5.1. Design Concept, Basic Flow Physics, and Principle of Operation; 2.5.2. Mesh and Metal Type; 2.5.3. Advantages and Disadvantages; 2.5.4. Storable Propellant Historical Examples; 2.5.4.1. Space Experiments; 2.5.4.2. Vehicles and Missions; 2.5.5. Cryogenic Propellant Historical Examples; 2.6. Propellant Management Device Combinations; 2.7. NASA's Current Needs; Chapter 3: Influential Factors and Physics-Based Modeling of Liquid Acquisition Devices; 3.1. 1-g One Dimensional Simplified Pressure Drop Model 3.2. The Room Temperature Bubble Point Pressure3.2.1. Assumptions; 3.2.2. Bubble Point Model Derivation; 3.2.3. Types of Bubble Point Experiments; 3.2.4. Surface Tension Model; 3.2.5. Specifying the Effective Pore Diameter; 3.2.6. Previously Reported Bubble Points; 3.3. Hydrostatic Pressure Drop; 3.4. Flow-Through-Screen Pressure Drop; 3.4.1. Model Derivation; 3.4.2. Model Parameters and Flow-Through-Screen Experiment; 3.4.3. Historical Data and Trends; 3.5. Frictional and Dynamic Pressure Drop; 3.6. Wicking Rate; 3.6.1. Model Derivation; 3.6.2. Wicking Rate Experiment 3.6.3. Historical Data and Trends3.7. Screen Compliance; 3.7.1. Model Derivation and Screen Compliance Experiment; 3.7.2. Historical Data and Trends; 3.8. Material Compatibility; 3.9. The Room Temperature Reseal Pressure Model; 3.9.1. Model Derivation; 3.9.2. Historical Data and Trends; 3.9.3. Specifying the Reseal Diameter; 3.10. Pressurant Gas Type; 3.11. Concluding Remarks and Implications for Cryogenic Propulsion Systems; Chapter 4: Room Temperature Liquid Acquisition Device Performance Experiments; 4.1. Pure Fluid Tests; 4.1.1. Scanning Electron Microscopy Analysis 4.1.2. Bubble Point Experimental Setup |
| Record Nr. | UNINA-9910817839403321 |
|
Hartwig Jason William
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| London, England : , : Academic Press, , 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Liquid rocket booster study . Volume II . Appendices 2-5 PPIP, transition plan, AMOS plan, environmental analysis : final report
| Liquid rocket booster study . Volume II . Appendices 2-5 PPIP, transition plan, AMOS plan, environmental analysis : final report |
| Pubbl/distr/stampa | San Diego, California : , : General Dynamics, Space Systems Division, , [1989] |
| Descrizione fisica | 1 online resource (various pagings) : illustrations |
| Collana | NASA-CR |
| Soggetto topico |
Space vehicles - Propulsion systems
Liquid propellant rockets - Fuel systems |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Liquid rocket booster study |
| Record Nr. | UNINA-9910715950503321 |
| San Diego, California : , : General Dynamics, Space Systems Division, , [1989] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Liquid rocket engine : thrust chamber parametric modeling / / Rene Nardi Rezende
| Liquid rocket engine : thrust chamber parametric modeling / / Rene Nardi Rezende |
| Autore | Rezende Rene Nardi |
| Pubbl/distr/stampa | Warrendale, Pennsylvania : , : SAE International, , [2019] |
| Descrizione fisica | 1 online resource (158 pages) : illustrations |
| Disciplina | 629.475 |
| Soggetto topico |
Space vehicles - Propulsion systems
Rockets (Aeronautics) |
| ISBN |
0-7680-9334-1
1-5231-2415-6 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910793728603321 |
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Rezende Rene Nardi
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| Warrendale, Pennsylvania : , : SAE International, , [2019] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Liquid rocket engine : thrust chamber parametric modeling / / Rene Nardi Rezende
| Liquid rocket engine : thrust chamber parametric modeling / / Rene Nardi Rezende |
| Autore | Rezende Rene Nardi |
| Pubbl/distr/stampa | Warrendale, Pennsylvania : , : SAE International, , [2019] |
| Descrizione fisica | 1 online resource (158 pages) : illustrations |
| Disciplina | 629.475 |
| Soggetto topico |
Space vehicles - Propulsion systems
Rockets (Aeronautics) |
| ISBN |
0-7680-9334-1
1-5231-2415-6 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910828228403321 |
|
Rezende Rene Nardi
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| Warrendale, Pennsylvania : , : SAE International, , [2019] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
