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 | ||
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 |
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 | ||
London, England : , : Academic Press, , 2016 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
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 |
Rezende Rene Nardi | ||
Warrendale, Pennsylvania : , : SAE International, , [2019] | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
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 | ||
Warrendale, Pennsylvania : , : SAE International, , [2019] | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Rocket and spacecraft propulsion : principles, practice and new developments / Martin J.L. Turner |
Autore | Turner, Martin J. L., 1942- |
Edizione | [2nd ed.] |
Pubbl/distr/stampa | Berlin ; New York : Springer |
Descrizione fisica | xxii, 313 p., [15] p. of plates : ill. (some col.) ; 25 cm |
Disciplina | 629.475 |
Collana | Springer-Praxis books in astronautical engineering |
Soggetto topico |
Space vehicles - Propulsion systems
Rockets (Aeronautics) Rocketry |
ISBN | 3540221905 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNISALENTO-991001804869707536 |
Turner, Martin J. L., 1942- | ||
Berlin ; New York : Springer | ||
Materiale a stampa | ||
Lo trovi qui: Univ. del Salento | ||
|
Rocket propellant handbook / Boris Kit , Douglas S. Evered. |
Autore | Kit, Boris |
Pubbl/distr/stampa | New York : The Macmillan company, 1960 |
Descrizione fisica | 354 p. : ill. ; 24 cm |
Disciplina | 629.475 |
Soggetto non controllato | Razzi - Propulsione |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | ita |
Record Nr. | UNINA-990000049910403321 |
Kit, Boris | ||
New York : The Macmillan company, 1960 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Rocket propulsion elements : an introduction to the engineering of rockets / George P. Sutton |
Autore | Sutton, George Paul |
Edizione | [6. ed] |
Pubbl/distr/stampa | New York, : Wiley, 1992 |
Descrizione fisica | X, 636 p. : ill. ; 24 cm. |
Disciplina | 629.475 |
ISBN | 04-7152-938-9 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNICAMPANIA-SUN0038229 |
Sutton, George Paul | ||
New York, : Wiley, 1992 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Vanvitelli | ||
|
Rocket propulsion elements : an introduction to the engineering of rockets / George P. Sutton |
Autore | Sutton, George Paul |
Edizione | [6. ed] |
Pubbl/distr/stampa | New York, : Wiley, 1992 |
Descrizione fisica | X, 636 p. : ill. ; 24 cm |
Disciplina | 629.475 |
ISBN | 04-7152-938-9 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Titolo uniforme | |
Record Nr. | UNICAMPANIA-VAN0038229 |
Sutton, George Paul | ||
New York, : Wiley, 1992 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Vanvitelli | ||
|
Rocket propulsion elements : a introduction to the engineering of rockets / George P. Sutton |
Autore | Sutton, George P. |
Edizione | [3.ed.] |
Pubbl/distr/stampa | New York : J. Wiley and sons, 1963 |
Descrizione fisica | VII, 464 p. : ill. ; 23 cm |
Disciplina | 629.475 |
Soggetto non controllato | Propulsione a razzo |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | ita |
Record Nr. | UNINA-990000025270403321 |
Sutton, George P. | ||
New York : J. Wiley and sons, 1963 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Spacecraft propulsion / Charles D. Brown |
Autore | Brown, Charles D., 1930- |
Pubbl/distr/stampa | Washington, DC : American Institute of Aeronautics and Astronautics, 1996 |
Descrizione fisica | xiv, 224 p. : ill. ; 24 cm. + 1 floppy |
Disciplina | 629.475 |
Collana | AIAA education series |
Soggetto topico | Space vehicles - Propulsion systems |
ISBN | 1563471280 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Record Nr. | UNISALENTO-991004120289707536 |
Brown, Charles D., 1930- | ||
Washington, DC : American Institute of Aeronautics and Astronautics, 1996 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. del Salento | ||
|