Modeling the Hall Thruster [electronic resource].
- Washington, D.C. : United States. Dept. of Energy. Office of Energy Research, 1998.
Oak Ridge, Tenn. : Distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy.
- Additional Creators:
- Princeton University. Plasma Physics Laboratory, United States. Department of Energy. Office of Energy Research, and United States. Department of Energy. Office of Scientific and Technical Information
- Restrictions on Access:
- Free-to-read Unrestricted online access
- The acceleration of the plasma in the Hall thruster to supersonic velocities is examined by the use of a steady state model. Flows that are smooth across the sonic transition plane are found. The possibility of generating flows in which the acceleration across the sonic plane is abrupt, is also studied.
- Report Numbers:
- E 1.99:cfp-3934
- Other Subject(s):
- Published through SciTech Connect.
American Institute of Aeronautics and Astronautics (AIAA) 34th Joint Propulsion, Cleveland, Ohio, July 13-15, 1998.
Fisch, N.J.; Fruchtman, A.
- Funding Information:
View MARC record | catkey: 14742888