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Rapid melt/quench furnace using commercially available hardwareThis report describes an off-the-shelf Orbital Tube Welder that can be easily used to melt and resolidify almost any electrically conductive material. This can be done on a KC-135 Aircraft within the microgravity period of one parabola. Melt sizes 3 mm diameter by 10 mm length and larger are feasible with most if not all materials. A highly reproducible, controlled, programmable heat and cool cycle can be provided. Sample measurements would have to be developed and could be as sophisticated or as simple as desired. These could include: optical and thermocouple temperature measurements, Peltier pulser for marking the solidification fronts, dimensional changes and whatever. Sample heat flows could be fixed over a very wide range being limited mostly by the cooling period, the desired sample size, and the 20 sec microgravity period of the KC-135 Aircraft parabola.
Document ID
19870010998
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Poorman, Richard M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1987
Subject Category
Materials Processing
Report/Patent Number
NASA-TM-86590
NAS 1.15:86590
Report Number: NASA-TM-86590
Report Number: NAS 1.15:86590
Accession Number
87N20431
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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