Theoretical and Numerical Analysis of Discharge Characteristics in Pulsed Electromagnetic Accelerators

Article Preview

Abstract:

Discharge is critical physical process in pulsed electromagnetic accelerators for arc plasma jet device, and its characteristics directly determines the accelerator performance. The mechanisms of discharge plasma and flow in the accelerator are analyzed by magnetohydrodynamics (MHD). The model is coupled with electric circuit model based on weakly nonideal plasma conductivity and ablation model. Calculation results show that there is some nonideal plasma region which has important effects on electrical conductivity; most ablated gases are ionized at the half cycle of the discharge time and are accelerated by Lorentz force to high exhaust velocity; electrical conductivity, plasma temperature and density are increasing with discharge energy unleashed, and gradually reduce in the post-discharge.

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 765-767)

Pages:

805-808

Citation:

Online since:

September 2013

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] K. A. Polzin, J. Propuls. Power. 27/3 (2011) 513.

Google Scholar

[2] S.S. Bushman, R.L. Burton J. Propuls. Power 17/5 (2001) 959.

Google Scholar

[3] N.Z. Gatsonis, J. Zwahlen, A. Wheelock, E.J. Pencil, H. Kamhawi, J. Propuls. Power 20/2 (2004) 243.

Google Scholar

[4] M. Keidar, I.D. Boyd I. I, IEEE Trans. Plasma Sci 28/2 (2000) 376.

Google Scholar

[5] M. Keidar, I.D. Boyd, J. Luke, C. Phipps, J. Appl. Phys 96/1 (2004) 49.

Google Scholar

[6] M. Keidar, L.D. Boyd, E. Antonsen, G.G. Spanjers, J. Propuls. Power 20/6 (2004) 961.

Google Scholar

[7] R.J. Zollweg, R.W. Liebermann, J. Appl. Phys 62/19 (1987) 3621.

Google Scholar

[8] Y.G. Mikellides, Ph.D. Thesis, Ohio State University, American, (1999).

Google Scholar

[9] E. L. Antonsen, R. L. Burton, G. A. Reed, G.G. Spanjers, J. Propuls. Power 21/5 (2005) 887.

Google Scholar

[10] R.J. Vondra, K. Thomassen, A. Solbes, J. Spacecraft Rocket 7/12 (1970): 1402.

Google Scholar