Accession Number : AD0884516
Title : AHP Cylinder Fabrication - LTV Carbon-Carbon Composite.
Descriptive Note : Final rept. Mar-Dec 70,
Corporate Author : LTV AEROSPACE CORP DALLAS TX MISSILES AND SPACE DIV
Personal Author(s) : Forcht, B. A.
Report Date : MAR 1971
Pagination or Media Count : 54
Abstract : Two 9 inch diameter, 15 inch long cylinders with a 1/2 inch wall were fabricated.Based on the results of the preceding carbon- arbon investigation, the R-120phenolic, WCA GRAPHITE CLOTH SYSTEM WITH FOUR FURFURYL ALCOHOL IMPREGNATIONS ANDREPYROLYZATION STEPS WAS USED. Flat panels were processed with the cylindersand characterized by mechanical and physical testing. These cylinders exhibitedimproved mechanical properties compared to those of the 6 inch diametercylinders fabricated in the preceding carbon-carbon investigation. One cylinderand test specimen, machined from the second cylinder, were forwarded to theAir Force for testing in the joint SAMSO/AFML/ FWL/Aerospace screening taskof the SAMSO Advanced Heatshield Program (AHP). (Author, modified-PL)
Descriptors : *GRAPHITE), (*COMPOSITE MATERIALS, (*HEAT SHIELDS, COMPOSITE MATERIALS), CARBON FIBERS, PHENOLIC PLASTICS, PYROLYSIS, CYLINDRICAL BODIES, MANUFACTURING, REINFORCED PLASTICS.
Subject Categories : Laminates and Composite Materials
Distribution Statement : APPROVED FOR PUBLIC RELEASE