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2200 C oxidizing atmosphere furnace for space manufacturingThe design of a high temperature furnace is presented which uses electrically conducting ceramic oxide heating elements. The heating elements are made of either thoria or stabilized zirconia which become conductive when preheated to 700 to 1000 C. These heater elements can be operated to 2200 C in oxidizing or inert atmospheres. The furnace is being designed to have a temperature which can be controlled to within 11 C. By a replacement of the heater element, the working cavity can be changed from isothermal to a cavity with a selected specific axial temperature gradient of up to 200 C per centimeter. This furnace concept is appropriate for the growth of crystals which might be grown best in an oxidizing atmosphere such as sapphire (melting point 2040 C), yttrium aluminum garnet (1970 C) or yttrium orthoaluminate (1875 C).
Document ID
19740036116
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Halbach, C. R.
Page, R. J.
(ARTCOR Irvine, Calif., United States)
Arthur, P. D.
(California, University Irvine, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1974
Subject Category
Machine Elements And Processes
Report/Patent Number
AIAA PAPER 74-154
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Washington, DC
Start Date: January 30, 1974
End Date: February 1, 1974
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
74A18866
Funding Number(s)
CONTRACT_GRANT: NAS8-29769
Distribution Limits
Public
Copyright
Other

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