BPT Hall Thruster Plume Characteristics
Author | : Kristi H. De Grys |
Publisher | : |
Total Pages | : |
Release | : 1999 |
Genre | : |
ISBN | : |
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Author | : Kristi H. De Grys |
Publisher | : |
Total Pages | : |
Release | : 1999 |
Genre | : |
ISBN | : |
Author | : Kevin D. Diamant |
Publisher | : |
Total Pages | : |
Release | : 2003 |
Genre | : |
ISBN | : |
Author | : Dan M. Goebel |
Publisher | : John Wiley & Sons |
Total Pages | : 528 |
Release | : 2008-12-22 |
Genre | : Technology & Engineering |
ISBN | : 0470436263 |
Throughout most of the twentieth century, electric propulsion was considered the technology of the future. Now, the future has arrived. This important new book explains the fundamentals of electric propulsion for spacecraft and describes in detail the physics and characteristics of the two major electric thrusters in use today, ion and Hall thrusters. The authors provide an introduction to plasma physics in order to allow readers to understand the models and derivations used in determining electric thruster performance. They then go on to present detailed explanations of: Thruster principles Ion thruster plasma generators and accelerator grids Hollow cathodes Hall thrusters Ion and Hall thruster plumes Flight ion and Hall thrusters Based largely on research and development performed at the Jet Propulsion Laboratory (JPL) and complemented with scores of tables, figures, homework problems, and references, Fundamentals of Electric Propulsion: Ion and Hall Thrusters is an indispensable textbook for advanced undergraduate and graduate students who are preparing to enter the aerospace industry. It also serves as an equally valuable resource for professional engineers already at work in the field.
Author | : J. Leon Shohet |
Publisher | : CRC Press |
Total Pages | : 3082 |
Release | : 2016-12-12 |
Genre | : Technology & Engineering |
ISBN | : 1351204939 |
Technical plasmas have a wide range of industrial applications. The Encyclopedia of Plasma Technology covers all aspects of plasma technology from the fundamentals to a range of applications across a large number of industries and disciplines. Topics covered include nanotechnology, solar cell technology, biomedical and clinical applications, electronic materials, sustainability, and clean technologies. The book bridges materials science, industrial chemistry, physics, and engineering, making it a must have for researchers in industry and academia, as well as those working on application-oriented plasma technologies. Also Available Online This Taylor & Francis encyclopedia is also available through online subscription, offering a variety of extra benefits for researchers, students, and librarians, including: Citation tracking and alerts Active reference linking Saved searches and marked lists HTML and PDF format options Contact Taylor and Francis for more information or to inquire about subscription options and print/online combination packages. US: (Tel) 1.888.318.2367; (E-mail) [email protected] International: (Tel) +44 (0) 20 7017 6062; (E-mail) [email protected]
Author | : C. Michael Tierney |
Publisher | : |
Total Pages | : 402 |
Release | : 1995 |
Genre | : Electronic dissertations |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 594 |
Release | : 2001 |
Genre | : Airplanes |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 522 |
Release | : 1999 |
Genre | : Airplanes |
ISBN | : |
Author | : Iain D. Boyd |
Publisher | : |
Total Pages | : |
Release | : 2000 |
Genre | : |
ISBN | : |
Author | : K. Kannenberg |
Publisher | : |
Total Pages | : |
Release | : 2001 |
Genre | : |
ISBN | : |
Author | : Yassir Azziz |
Publisher | : |
Total Pages | : 230 |
Release | : 2007 |
Genre | : |
ISBN | : |
(Cont.) However, comparison of plume simulation and experimental results at a non-zero background pressure showed deficiencies in the collision model of the plume simulation. An analytical expression for current density obtained using a elf-similar plume model was compared to extrapolated current density at zero pressure and showed good agreement. In addition, an analytical model derived for current density of source ion collisions with neutrals was consistent with experimental measurements and confirms the deficiencies in the simulation's collision model. In summary, experimental, numerical and analytical results indicate that the method of determining in-orbit plume divergence from laboratory measurements is valid and can be used to integrate Hall thrusters with the spacecraft.