Accession Number : ADA302550

Title :   NASA/Aircraft Industry Standard Specification for Graphite Fiber/Toughened Thermoset Resin Composite Material.

Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION HAMPTON VA LANGLEY RESEARCH CEN TER

PDF Url : ADA302550

Report Date : JUN 1985

Pagination or Media Count : 59

Abstract : This specification establishes requirements for qualification and batch acceptance of a carbon fiber toughened thermoset resin prepreg that will provide a laminate with service temperature from -650F to +2OO0F when cured in an autoclave at temperatures not higher than 3500F and at pressures no greater than 100 psi.

Descriptors :   *FIBER REINFORCED COMPOSITES, *TOUGHNESS, *THERMOSETTING PLASTICS, TENSILE STRENGTH, AIRCRAFT INDUSTRY, SPECIFICATIONS, COMPOSITE MATERIALS, MILITARY STANDARDS, LAMINATES, TEST METHODS, GRAPHITE, QUALITY ASSURANCE, CURING, PREPREGS, COMPRESSIVE STRENGTH, VISCOSITY, SHIPPING CONTAINERS, DELAMINATION, SHEAR STRENGTH, PACKING MATERIALS.

Subject Categories : Laminates and Composite Materials
      Plastics

Distribution Statement : APPROVED FOR PUBLIC RELEASE