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Non-ambipolar Electron Source
Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNC06CB42C
Agency Tracking Number: 050300
Amount:
$100,000.00
Phase:
Phase I
Program:
STTR
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Timeline
Solicitation Year:
N/A
Award Year:
2006
Award Start Date (Proposal Award Date):
N/A
Award End Date (Contract End Date):
N/A
Small Business Information
8123 Forsythia Street Suite 140, Madison, WI, 53562
DUNS:
612389572
HUBZone Owned:
N
Woman Owned:
N
Socially and Economically Disadvantaged:
N
Principal Investigator
Name: Noah Hershkowitz
Title: Principal Investigator
Phone: () -
Email: hershkowitz@engr.wisc.edu
Title: Principal Investigator
Phone: () -
Email: hershkowitz@engr.wisc.edu
Business Contact
Name: Gregory Piefer
Title: Business Official/President
Phone: (608) 345-3779
Email: grpiefer@wisc.edu
Title: Business Official/President
Phone: (608) 345-3779
Email: grpiefer@wisc.edu
Research Institution
Name: University of Wisconsin-Madison
Contact: Stepahnie Gray
Address: 301 N. Whitney Way
Madison, WI, 53706
Phone: (608) 263-4970
Type: Nonprofit college or university
Contact: Stepahnie Gray
Address: 301 N. Whitney Way
Madison, WI, 53706
Phone: (608) 263-4970
Type: Nonprofit college or university
Abstract
A device to produce electron beams from magnetized plasma created with rf fields combined with electron extraction by electron sheaths is proposed. The source can provide electrons for neutralizing positive ion beams emerging from ion thrusters or as a generic electron source. With hollow cathode sources currently employed to provide neutralizing electrons, operation is limited in time and/or current density by cathode deterioration. RF electron sources provide an alternative approach that does not consume electrode material. The current from this Non-ambipolar Electron Source (NES) exceeds the current normally extracted from conventional rf plasma sources by a factor of (mi/me)1/2 where mi and me are the ion and electron mass. Ions are lost to a negatively biased conducting cylinder with area Ai chosen to be Ai ≥ (mi/me)1/2 *Ae where Ae is the electron extraction area. Slots in the conducting cylinder allow the cylinder to serve as a Faraday shield to reduce capacitive coupling from the antenna to the plasma. Proposed phase 1 design improvements should result in electron currents comparable to hollow cathode sources with lower neutral gas flow in the inductive discharge phase and higher currents with helicon operation. Phase 2 will develop prototype sources suitable for spacecraft testing. * Information listed above is at the time of submission. *