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Air-Cored Linear Induction Motor for Earth-to-Orbit SystemsThe need for lowering the cost of Earth-to-Orbit (ETO) launches has prompted consideration of electromagnetic launchers. A preliminary design based on the experience gained in an advanced type of coilgun and on innovative ideas shows that such a launcher is technically feasible with almost off-the-shelf components.
Document ID
19960050143
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Zabar, Zivan (Polytechnic Univ. Brooklyn, NY United States)
Levi, Enrico (Polytechnic Univ. Brooklyn, NY United States)
Birenbaum, Leo (Polytechnic Univ. Brooklyn, NY United States)
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
96N34250
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19960050126Collected WorksThird International Symposium on Magnetic Suspension Technology
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