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Design and fabrication of a super alloy thermal protection systemA lightweight metallic TPS was designed, and two test articles were fabricated, one from Haynes 188 and one from Rene 41. A baseline TPS concept, selected at the beginning of the program, consisted of a Haynes 25 corrugation-stiffened beaded skin surface panel, a specially designed support system, and an insulation system. By optimizing the structure for the design loads and by chem-milling to remove material not needed, the mass of the baseline surface panel was reduced 25%, and the mass of the support structure was reduced 50%. The insulation system mass was reduced 40% by using two types of insulation, each suited to its temperature range, and by eliminating a foul bag which encapsulated the baseline insulation system. These reductions resulted in an overall 35% reduction in mass of the Haynes 188 panel from the baseline Haynes 25 design. Similar reductions were achieved with the Rene 41 system.
Document ID
19790013268
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Varisco, A.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Wolter, W.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Bell, P.
(Grumman Aerospace Corp. Bethpage, NY, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Publication Information
Publication: NASA. Langley Res. Center Recent Advan. in Structures for Hypersonic Flight, Pt. 2
Subject Category
Structural Mechanics
Accession Number
79N21439
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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