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Development, fabrication and evaluation of composite thermal engine insulationFoil enclosure configurations of 10 variations were fabricated and evaluated. A discussion of the thermal protection system panel design includes: (1) description of 3DSX/foil concept, (2) design environment, (3) material selection, (4) fabrication enclosure, (5) structural design, (6) thermal sizing, and (7) weight analysis. The structural design study includes foil evaluation, venting pressure loads, thermomechanical behavior, and enclosure venting (burst) pressure tests. Results of experimental demonstrations of performance and reuse capabilities are given for both thermal and acoustic testing.
Document ID
19730024725
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 2, 2013
Publication Date
September 1, 1973
Subject Category
Materials, Nonmetallic
Report/Patent Number
AVSD-0268-73-RR
NASA-CR-124457
Report Number: AVSD-0268-73-RR
Report Number: NASA-CR-124457
Accession Number
73N33458
Funding Number(s)
CONTRACT_GRANT: NAS8-29061
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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