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タイトルPlasma Liner Research for MTF at NASA Marshall Space Flight Center
著者(英)Knapp, C. E.; Wu, S. T.; Kirkpatrick, R. C.; Lee, M.; Rodgers, Stephen L.; Thio, Y. C. F.; Martin, A.; Turchi, P. J.; Cassibry, J. T.; Eskridge, R.; Smith, J.
著者所属(英)NASA Marshall Space Flight Center
発行日2002-01-01
言語eng
内容記述The current research effort at NASA Marshall Space Flight Center (MSFC) in MTF is directed towards exploring the critical physics issues of potential embodiments of MTF for propulsion, especially standoff drivers involving plasma liners for MTF. There are several possible approaches for forming plasma liners. One approach consists of using a spherical array of plasma jets to form a spherical plasma shell imploding towards the center of a magnetized plasma, a compact toroid. Current experimental plan and status to explore the physics of forming a 2-D plasma liner (shell) by merging plasma jets are described. A first-generation coaxial plasma guns (Mark-1) to launch the required plasma jets have been built and tested. Plasma jets have been launched reproducibly with a low jitter, and velocities in excess of 50 km/s for the leading edge of the plasma jet. Some further refinements are being explored for the plasma gun, Successful completion of these single-gun tests will be followed by an experimental exploration of the problems of launching a multiple number of these jets simultaneously to form a cylindrical plasma liner.
NASA分類Spacecraft Propulsion and Power
権利No Copyright


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