The fusion Z-pinch experiment device produces a 0.3 cm radius by 50 cm-long Z pinch between the end of the inner electrode of a coaxial plasma gun and an end wall 50 cm away. The plasma column is stabilized for thousands of instability growth times by an embedded radially sheared axial plasma flow. To investigate the effect of end wall design on Z-pinch plasma behavior, the solid end wall with a central exhaust port is replaced with a spoked end wall with a solid hub. While the Z-pinch plasma behavior was largely unaffected, the plasma exhausted from the Z-pinch provides an experimental platform to study magnetic confinement and detachment. Current and density signals are compared between two cases: a low energy and a high energy case. Plasma is found to be frozen-in flux in the Z-pinch assembly region. The exhaust of plasma from the flux conserving region is found to be dependent on the ratio of plasma ram and thermal pressures to the local magnetic pressure, calculated from an equilibrium model at the end wall. Plasma exhaust is observed to increase with the spoked end wall only for the high energy conditions as its ratio of ram and thermal pressures to the magnetic pressure increases.
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September 2020
Research Article|
September 25 2020
Plasma exhaust in a sheared-flow-stabilized Z pinch
E. L. Claveau
;
E. L. Claveau
a)
1
Aerospace and Energetics Research Program, University of Washington
, Seattle, Washington 98195, USA
a)Author to whom correspondence should be addressed: [email protected]
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U. Shumlak
;
U. Shumlak
1
Aerospace and Energetics Research Program, University of Washington
, Seattle, Washington 98195, USA
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B. A. Nelson;
B. A. Nelson
2
Zap Energy, Inc
., Seattle, Washington 98104, USA
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E. G. Forbes
;
E. G. Forbes
1
Aerospace and Energetics Research Program, University of Washington
, Seattle, Washington 98195, USA
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A. D. Stepanov
;
A. D. Stepanov
1
Aerospace and Energetics Research Program, University of Washington
, Seattle, Washington 98195, USA
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T. R. Weber;
T. R. Weber
1
Aerospace and Energetics Research Program, University of Washington
, Seattle, Washington 98195, USA
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Y. Zhang
;
Y. Zhang
2
Zap Energy, Inc
., Seattle, Washington 98104, USA
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H. S. McLean
H. S. McLean
3
Lawrence Livermore National Laboratory
, Livermore, California 94550, USA
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E. L. Claveau
1,a)
U. Shumlak
1
B. A. Nelson
2
E. G. Forbes
1
A. D. Stepanov
1
T. R. Weber
1
Y. Zhang
2
H. S. McLean
3
1
Aerospace and Energetics Research Program, University of Washington
, Seattle, Washington 98195, USA
2
Zap Energy, Inc
., Seattle, Washington 98104, USA
3
Lawrence Livermore National Laboratory
, Livermore, California 94550, USA
a)Author to whom correspondence should be addressed: [email protected]
Phys. Plasmas 27, 092510 (2020)
Article history
Received:
June 14 2020
Accepted:
August 31 2020
Citation
E. L. Claveau, U. Shumlak, B. A. Nelson, E. G. Forbes, A. D. Stepanov, T. R. Weber, Y. Zhang, H. S. McLean; Plasma exhaust in a sheared-flow-stabilized Z pinch. Phys. Plasmas 1 September 2020; 27 (9): 092510. https://doi.org/10.1063/5.0018429
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