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Silica heat shield sizingThe sensitivity of silica heat shield requirements to gap width, tile edge radius, and heat transfer distribution within tile gaps was investigated. A two-dimensional thermal model was modified and used to determine the effect of two dimensional heat transfer distributions at high temperature reusable surface insulation edges on shuttle thermal protection system (TPS) requirements. The sensitivity of TPS requirements to coating thickness, emissivity, substructure thickness, and changes in gap heating for several locations on shuttle was also studied. An inverse solution technique was applied to temperature data obtained in the Ames 20 MW turbulent duct in order to examine the effect of tile edge radius on TPS requirements. The derived heating values were then used to predict TPS requirements. Results show that increasing tile radius reduces TPS requirements.
Document ID
19770010457
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ebbesmeyer, L. H.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Christensen, H. E.
(McDonnell-Douglas Astronautics Co. Saint Louis, MO, United States)
Date Acquired
September 3, 2013
Publication Date
July 24, 1975
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
MDC-E1343
NASA-CR-151962
Report Number: MDC-E1343
Report Number: NASA-CR-151962
Accession Number
77N17401
Funding Number(s)
CONTRACT_GRANT: NAS2-7897
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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