Energetic Ion Mitigation Methodology for High Power Plasma Thruster Cathodes

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$199,725.00
Award Year:
2013
Program:
SBIR
Phase:
Phase I
Contract:
NNX13CC13C
Agency Tracking Number:
125646
Solicitation Year:
2012
Solicitation Topic Code:
E1.01
Solicitation Number:
n/a
Small Business Information
ElectroDynamic Applications, Inc.
MI, Ann Arbor, MI, 48105-1570
Hubzone Owned:
N
Minority Owned:
Y
Woman Owned:
N
Duns:
610511334
Principal Investigator:
Christopher Davis
Senior Engineer
(734) 786-1434
davis@edapplications.com
Business Contact:
Jonathan Zagel
Business Official
(734) 786-1434
info@edapplications.com
Research Institution:
Stub




Abstract
The presence of energetic ions, that appear under high cathode current operation, stand as a showstopper to the realization of high power electric propulsion. Physical barriers such as the use of carbon electrodes (e.g. NEXT) are no longer sufficient as ion energies measured greatly exceed the sputter threshold of even carbon. Unless this problem is addressed, the prospect of inadequate life looms. The benefits of high power electric propulsion missions supporting human operations in particular would be left unfulfilled.This effort aims to fully characterize the conditions under which energy ions occur by documenting ion energy spectra over a range of representative operating conditions. At these conditions, the effort will implement two novel methods of essentially defeating the energetic ion production mechanism: 1) magnetic shorting and 2) gas injection. While the concept of injecting gas to quench energetic ion production has been demonstrated in the past, we take the approach a step further by 1) elucidating the mechanism by which gas injection actually quenches energetic ion production and 2) implementing a novel gas applicator that would conserve propellant thereby allowing for gas implementation without a significant efficiency sacrifice. Past studies have shown that energetic ions form under conditions of high current. No satisfactory understanding of how these are formed or how to mitigate has been communicated. This effort aims to address both issues. The focus of the proposed effort directly addresses a problem that stands in the critical path for the development of high power electric propulsion. Without a solution to the energetic ion lifetime issue, it is difficult to imagine the actual implementation of high power electric propulsion for actual missions. This proposed effort aims to generate a methodology and apparatus for the elimination of energy ions in high current cathodes.

* information listed above is at the time of submission.

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