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Magnetic levitation systems for future aeronautics and space research and missionsThe objectives, advantages, and research needs for several applications of superconducting magnetic levitation to aerodynamics research, testing, and space-launch are discussed. Applications include very large-scale magnetic balance and suspension systems for high alpha testing, support interference-free testing of slender hypersonic propulsion/airframe integrated vehicles, and hypersonic maglev. Current practice and concepts are outlined as part of a unified effort in high magnetic fields R&D within NASA. Recent advances in the design and construction of the proposed ground-based Holloman test track (rocket sled) that uses magnetic levitation are presented. It is protected that ground speeds of up to Mach 8 to 11 at sea-level are possible with such a system. This capability may enable supersonic combustor tests as well as ramjet-to-scramjet transition simulation to be performed in clean air. Finally a novel space launch concept (Maglifter) which uses magnetic levitation and propulsion for a re-usable 'first stage' and rocket or air-breathing combined-cycle propulsion for its second stage is discussed in detail. Performance of this concept is compared with conventional advanced launch systems and a preliminary concept for a subscale system demonstration is presented.
Document ID
19960023619
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Blankson, Isaiah M.
(NASA Headquarters Washington, DC United States)
Mankins, John C.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1996
Publication Information
Publication: Transportation Beyond 2000: Technologies Needed for Engineering Design
Subject Category
Mechanical Engineering
Accession Number
96N26311
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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