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Evaluation of the energy transfer in the char zone during ablation. Part 2: In-depth response of ablative composites, volume 1The decomposition of ablative composites is described along with the transport phenomena of pyrolysis gases which result from the decomposition of these plastics as they flow through the porous char of char-forming ablators. The pyrolysis products are those formed by the thermal degradation of nylon-phenolic resin and silicone elastomer composites. Emphasis is placed on the nature and extent of chemical reactions of the pyrolysis products and the char, along with the energy absorbed by the combined pyrolysis and char zone. Chemical reactions with thermodynamically consistent kinetic data are determined in order to develop a realistic analysis for predicting the thermal performance of ablative heat shields.
Document ID
19750017018
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Pike, R. W.
(Louisiana State Univ. Baton Rouge, LA, United States)
Delvalle, E. G.
(Louisiana State Univ. Baton Rouge, LA, United States)
Date Acquired
September 3, 2013
Publication Date
December 15, 1974
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-132699
Report Number: NASA-CR-132699
Accession Number
75N25090
Funding Number(s)
CONTRACT_GRANT: NGR-19-001-016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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