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Castable thermal insulation for use as heat shieldsStructural members supporting the afterburners of high thrust rocket engines are subjected to extreme heating, along with severe vibration and high acceleration levels during early lift-off. Chemically-bonded, castable, zircon composite foams were developed and successfully tested to meet specific, laboratory simulated lift-off conditions.
Document ID
19750029953
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Mountvala, A. J.
Nakamura, H. H.
Rechter, H. L.
(IIT Research Institute Chicago, Ill., United States)
Date Acquired
August 8, 2013
Publication Date
November 1, 1974
Publication Information
Publication: American Ceramic Society Bulletin
Volume: 53
Subject Category
Nonmetallic Materials
Accession Number
75A14025
Funding Number(s)
CONTRACT_GRANT: NAS8-11333
Distribution Limits
Public
Copyright
Other

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