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Process modeling for carbon-phenolic nozzle materialsA thermochemical model based on the SINDA heat transfer program is developed for carbon-phenolic nozzle material processes. The model can be used to optimize cure cycles and to predict material properties based on the types of materials and the process by which these materials are used to make nozzle components. Chemical kinetic constants for Fiberite MX4926 were determined so that optimization of cure cycles for the current Space Shuttle Solid Rocket Motor nozzle rings can be determined.
Document ID
19890059620
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Letson, Mischell A.
(Morton Thiokol Huntsville, AL, United States)
Bunker, Robert C.
(Morton Thiokol Huntsville, AL, United States)
Remus, Walter M., III
(Morton Thiokol, Inc. Space Div., Huntsville, AL, United States)
Clinton, R. G.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1989
Subject Category
Composite Materials
Report/Patent Number
AIAA PAPER 89-2657
Accession Number
89A46991
Distribution Limits
Public
Copyright
Other

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