Abstract
A 9 cm cylindrical thruster with a ceramic channel exhibited performance comparable to the state-of-the-art Hall thrusters at low and moderate power levels. Significantly, its operation is not accompanied by large amplitude discharge low frequency oscillations. Preliminary experiments on a 2 cm cylindrical thruster suggest the possibility of a high performance micro Hall thruster.
| Original language | English (US) |
|---|---|
| DOIs | |
| State | Published - 2000 |
| Event | 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2000 - Huntsville, AL, United States Duration: Jul 16 2000 → Jul 19 2000 |
Other
| Other | 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2000 |
|---|---|
| Country/Territory | United States |
| City | Huntsville, AL |
| Period | 7/16/00 → 7/19/00 |
All Science Journal Classification (ASJC) codes
- Control and Systems Engineering
- Electrical and Electronic Engineering
- Mechanical Engineering
- Aerospace Engineering
- Space and Planetary Science
- Energy Engineering and Power Technology
Fingerprint
Dive into the research topics of 'A study of cylindrical Hall thruster for low power space applications'. Together they form a unique fingerprint.Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver