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Materials Property Definition and Generation for Carbon-Carbon and Carbon Phenolic MaterialsThe use of carbon phenolic and carbon-carbon materials in nozzle and exit cone designs has been historically plagued by the lack of reliable, statistically significant material property data. Property data are needed by designers to analyze thermal response and stress levels and develop designs with safety factors that assume high reliability at minimum weight penalties. This program is structured to provide the data necessary for thermal and stress modeling or tape-wrapped carbon phenolic and involute carbon-carbon components.

The work is initially directed at determining critical properties for analysis followed by evaluation of existing data and the determination of data deficiencies. New data will be generated in statistically significant quantities. Alternate materials will be selected and characterized and a final data book will be prepared.

Materials to be tested will be excised from Space Shuttle inlet throat, and exit cone billets and modified IUS and STAR 48 involute carbon-carbon exit cones; co-processed blocks. panels, and cylinders will also be tested. Morton Thiokol, Inc., is fabricating the Shuttle parts; Kaiser and Hitco are fabricating the IUS and STAR 48 components; and Southern Research will do the testing. Figure 1 outlines the program.
Document ID
19870057956
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
A R Canfield
(Thiokol (United States) Ogden, United States)
J R Mathis
(Thiokol (United States) Ogden, United States)
H S Starrett
(Southern Research Institute Durham, North Carolina, United States)
J R Koenig
(Southern Research Institute Durham, North Carolina, United States)
Date Acquired
August 13, 2013
Publication Date
June 29, 1987
Publication Information
Publication: 23rd Joint Propulsion Conference
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Composite Materials
Report/Patent Number
AIAA-87-1825
Meeting Information
Meeting: AIAA/SAE/ASME/ASEE 23rd Joint Propulsion Conference
Location: San Diego, CA
Country: US
Start Date: June 29, 1987
End Date: July 2, 1987
Sponsors: American Society of Mechanical Engineers, American Society For Engineering Education, American Institute of Aeronautics and Astronautics, Society of Automotive Engineers International
Accession Number
87A45230
Funding Number(s)
CONTRACT_GRANT: NAS8-36297
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Shear Stress
Rocket Motor
Thermal Response
Statistical Analysis
Thermal Conductivity
Space Shuttle
Thermal Expansion
Thermal Gravimetric Analysis
Compressive Strength
Material Properties
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