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Plasma Jet Injection of Angular Momentum in the Maryland Centrifugal Experiment

Award Information
Agency: Department of Energy
Branch: N/A
Contract: DE-FG02-05ER84189
Agency Tracking Number: 79317S05-I
Amount: $749,848.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: 32
Solicitation Number: DE-FG02-06ER06-09
Timeline
Solicitation Year: 2006
Award Year: 2006
Award Start Date (Proposal Award Date): N/A
Award End Date (Contract End Date): N/A
Small Business Information
11316 Smoke Rise Court
Fairfax Station, VA 22039
United States
DUNS: N/A
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 F. Witherspoon
 Dr.
 (703) 378-4882
 witherspoon@HyperV.com
Business Contact
 F. Witherspoon
Title: Dr.
Phone: (703) 378-4882
Email: witherspoon@HyperV.com
Research Institution
N/A
Abstract

The centrifugal confinement of plasma has great potential as a fusion device. In order to operate in the highest temperature and density regimes, angular momentum must be injected into the plasma without permitting the plasma to come into contact with a material surface. To accomplish this, the plasma must be injected at high velocity tangential to the direction of plasma rotation. In this project, angular momentum will be injected into a large centrifugally confined mirror plasma, using a two stage coaxial plasma accelerator with shaped electrodes. This process will allow the high velocity jets to efficiently couple to the target plasma. In Phase I, a prototype accelerator was designed and fabricated, and test-fired in the laboratory in preparation for injection experiments on a mirror machine plasma experiment. Simulations were performed that showed that high velocity, moderate mass slugs efficiently can indeed drive target plasma rotation. In Phase II, the plasma jet hardware will be installed on a large, centrifugally-confined, mirror plasma experiment, and extensive testing will be performed. The ideal set of parameters that will most effectively couple the jet momentum to the plasma rotation will be determined. The computational modeling will be benchmarked against these results. Commercial Applications and other Benefits as described by the awardee: The plasma jet technology should be applicable to commercial fusion power, refueling of magnetically confined plasmas, high specific-impulse thrusters for space propulsion, laboratory simulation of astrophysical jets, fast-pulsed power switching, and materials processing

* Information listed above is at the time of submission. *

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