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A multi-zone muffle furnace designA Multi-Zone Muffle-Tube Furnace was designed, built, and tested for the purpose of providing an in-house experience base with tubular furnaces for materials processing in microgravity. As such, it must not only provide the desired temperatures and controlled thermal gradients at several discrete zones along its length but must also be capable of sustaining the rigors of a Space Shuttle launch. The furnace is insulated to minimize radial and axial heat losses. It is contained in a water-cooled enclosure for purposes of dissipating un-wanted residual heat, keeping the outer surfaces of the furnace at a 'touch-safe' temperature, and providing a rugged housing. This report describes the salient features of the furnace, testing procedures and results, and concluding remarks evaluating the overall design.
Document ID
19930017822
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Rowe, Neil D.
(NASA Lewis Research Center Cleveland, OH, United States)
Kisel, Martin
(Analex Corp. Brook Park, OH., United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1993
Subject Category
Materials Processing
Report/Patent Number
NASA-TM-106153
NAS 1.15:106153
E-7837
Report Number: NASA-TM-106153
Report Number: NAS 1.15:106153
Report Number: E-7837
Accession Number
93N27011
Funding Number(s)
PROJECT: RTOP 694-03-0C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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