Abstract
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.
Original language | English (US) |
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DOIs | |
State | Published - 1998 |
Event | 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 1998 - Cleveland, United States Duration: Jul 13 1998 → Jul 15 1998 |
Other
Other | 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 1998 |
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Country/Territory | United States |
City | Cleveland |
Period | 7/13/98 → 7/15/98 |
All Science Journal Classification (ASJC) codes
- Energy Engineering and Power Technology
- Electrical and Electronic Engineering
- Mechanical Engineering
- Control and Systems Engineering
- Aerospace Engineering