Abstract
Current neutralizer technology is unsuited for extremely long duration missions. To date, hollow cathode technology has been the primary neutralization method for electric propulsion missions. However, the operational lifetime of a hollow cathode is limited by depletion of the barium insert and erosion of the thin-walled cathode. Electron cyclotron resonance (ECR) neutralizers are a promising solution to the lifetime problem. Relying on the resonant coupling of particle motion around a static magnetic field and an incident microwave, an ECR neutralizer generates a plasma from which electrons can be extracted. The neutralizer is electrodeless and does not rely on a depletable insert, thereby eliminating the most common failure modes of the hollow cathode. In this work, a high power, waveguide-fed ECR neutralizer was designed and built, and initial tests conducted. The system serves as a proof-of-concept model and, as such, was designed to be easily modifiable for future design iterations and investigations. This paper reports on initial tests of the neutralizer in which it was found to perform as expected. The neutralizer was tested at background pressures between 5×10-4 and 7×10-3 torr. Plasma ignition was noted with a minimal input power of 40 W. In addition, both low and high modes of operation were noted, with the high mode initiating at around 300 W. An extraction current of 2.45 A was achieved with 550 W of input power at 0.7 mtorr. In addition, a maximum extraction current of 2 A was achieved at 850 W and 1 mtorr. At this operating pressure, an increase in input power beyond 850 W did not result in an increase in the extraction current, indicating that a cutoff plasma density had been reached.
| Original language | English (US) |
|---|---|
| Title of host publication | Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference |
| Pages | 2884-2893 |
| Number of pages | 10 |
| State | Published - Dec 11 2007 |
| Event | 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference - Cincinnati, OH, United States Duration: Jul 8 2007 → Jul 11 2007 |
Publication series
| Name | Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference |
|---|---|
| Volume | 3 |
Other
| Other | 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference |
|---|---|
| Country | United States |
| City | Cincinnati, OH |
| Period | 7/8/07 → 7/11/07 |
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All Science Journal Classification (ASJC) codes
- Space and Planetary Science
Cite this
}
Design and testing of a high power electron cyclotron resonance neutralizer. / Edgar, Matthew C.; Bilén, Sven G.
Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference. 2007. p. 2884-2893 (Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference; Vol. 3).Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
TY - GEN
T1 - Design and testing of a high power electron cyclotron resonance neutralizer
AU - Edgar, Matthew C.
AU - Bilén, Sven G.
PY - 2007/12/11
Y1 - 2007/12/11
N2 - Current neutralizer technology is unsuited for extremely long duration missions. To date, hollow cathode technology has been the primary neutralization method for electric propulsion missions. However, the operational lifetime of a hollow cathode is limited by depletion of the barium insert and erosion of the thin-walled cathode. Electron cyclotron resonance (ECR) neutralizers are a promising solution to the lifetime problem. Relying on the resonant coupling of particle motion around a static magnetic field and an incident microwave, an ECR neutralizer generates a plasma from which electrons can be extracted. The neutralizer is electrodeless and does not rely on a depletable insert, thereby eliminating the most common failure modes of the hollow cathode. In this work, a high power, waveguide-fed ECR neutralizer was designed and built, and initial tests conducted. The system serves as a proof-of-concept model and, as such, was designed to be easily modifiable for future design iterations and investigations. This paper reports on initial tests of the neutralizer in which it was found to perform as expected. The neutralizer was tested at background pressures between 5×10-4 and 7×10-3 torr. Plasma ignition was noted with a minimal input power of 40 W. In addition, both low and high modes of operation were noted, with the high mode initiating at around 300 W. An extraction current of 2.45 A was achieved with 550 W of input power at 0.7 mtorr. In addition, a maximum extraction current of 2 A was achieved at 850 W and 1 mtorr. At this operating pressure, an increase in input power beyond 850 W did not result in an increase in the extraction current, indicating that a cutoff plasma density had been reached.
AB - Current neutralizer technology is unsuited for extremely long duration missions. To date, hollow cathode technology has been the primary neutralization method for electric propulsion missions. However, the operational lifetime of a hollow cathode is limited by depletion of the barium insert and erosion of the thin-walled cathode. Electron cyclotron resonance (ECR) neutralizers are a promising solution to the lifetime problem. Relying on the resonant coupling of particle motion around a static magnetic field and an incident microwave, an ECR neutralizer generates a plasma from which electrons can be extracted. The neutralizer is electrodeless and does not rely on a depletable insert, thereby eliminating the most common failure modes of the hollow cathode. In this work, a high power, waveguide-fed ECR neutralizer was designed and built, and initial tests conducted. The system serves as a proof-of-concept model and, as such, was designed to be easily modifiable for future design iterations and investigations. This paper reports on initial tests of the neutralizer in which it was found to perform as expected. The neutralizer was tested at background pressures between 5×10-4 and 7×10-3 torr. Plasma ignition was noted with a minimal input power of 40 W. In addition, both low and high modes of operation were noted, with the high mode initiating at around 300 W. An extraction current of 2.45 A was achieved with 550 W of input power at 0.7 mtorr. In addition, a maximum extraction current of 2 A was achieved at 850 W and 1 mtorr. At this operating pressure, an increase in input power beyond 850 W did not result in an increase in the extraction current, indicating that a cutoff plasma density had been reached.
UR - http://www.scopus.com/inward/record.url?scp=36749039690&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=36749039690&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:36749039690
SN - 1563479036
SN - 9781563479038
T3 - Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference
SP - 2884
EP - 2893
BT - Collection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference
ER -