Distribution Of Neutral Propellant From Electric Thrusters Onto Spacecraft Components
Distribution Of Neutral Propellant From Electric Thrusters Onto Spacecraft Components Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Distribution Of Neutral Propellant From Electric Thrusters Onto Spacecraft Components book. This book definitely worth reading, it is an incredibly well-written.
Ion-thruster Propellant Utilization by Harold R. Kaufman Pdf
The evaluation and understanding of maximum propellant utilization, with mercury used as the propellant are presented. The primary-electron region in the ion chamber of a bombardment thruster is analyzed at maximum utilization. The results of this analysis, as well as experimental data from a range of ion-chamber configurations, show a nearly constant loss rate for unionized propellant at maximum utilization over a wide range of total propellant flow rate. The discharge loss level of 1000 eV/ion was used as a definition of maximum utilization, but the exact level of this definition has no effect on the qualitative results and little effect on the quantitative results. There are obvious design applications for the results of this investigation, but the results are particularly significant whenever efficient throttled operation is required.
Author : United States. Superintendent of Documents Publisher : Unknown Page : 1504 pages File Size : 55,8 Mb Release : 1979 Category : United States ISBN : STANFORD:36105019598296
Fundamentals of Electric Propulsion by Dan M. Goebel,Ira Katz Pdf
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.
Rocket and Spacecraft Propulsion by Martin J. L. Turner Pdf
The revised edition of this practical, hands-on book discusses the launch vehicles in use today throughout the world, and includes the latest details on advanced systems being developed, such as electric and nuclear propulsion. The author covers the fundamentals, from the basic principles of rocket propulsion and vehicle dynamics through the theory and practice of liquid and solid propellant motors, to new and future developments. He provides a serious exposition of the principles and practice of rocket propulsion, from the point of view of the user who is not an engineering specialist.
Rocket Propulsion Elements by George P. Sutton Pdf
Concentrates on the subject of rock propulsion, its basic technology, performance and design rationale. Provides an introduction to the subject, an understanding of basic principles, a description of their physical mechanisms and designs, and an understanding of the application of rocket propulsion to flying vehicles.