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Electromechanical Dynamics Simulations of Superconducting LSM Rocket Launcher System in Attractive-ModeFurther feasibility study on a superconducting linear synchronous motor (LSM) rocket launcher system is presented on the basis of dynamic simulations of electric power, efficiency and power factor as well as the ascending motions of the launcher and rocket. The advantages of attractive-mode operation are found from comparison with repulsive-mode operation. It is made clear that the LSM rocket launcher system, of which the long-stator is divided optimally into 60 sections according to launcher speeds, can obtain high efficiency and power factor.
Document ID
19960050142
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Yoshida, Kinjiro
(Kyushu Univ. Fukuoka, Japan)
Hayashi, Kengo
(Kyushu Univ. Fukuoka, Japan)
Takami, Hiroshi
(Kyushu Univ. Fukuoka, Japan)
Date Acquired
September 6, 2013
Publication Date
July 1, 1996
Publication Information
Publication: Third International Symposium on Magnetic Suspension Technology
Volume: Part 2
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
96N34249
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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