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

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.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1985
Accession Number
ADA302550

Entities

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms
  • Biomedical
  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Acceptance Tests
  • Aircraft Industry
  • Aircrafts
  • Carbon Fibers
  • Commercial Aircraft
  • Composite Materials
  • Fabrication
  • Graphitic Materials
  • Liquid Chromatography
  • Materials Processing
  • Materials Testing
  • Measurement
  • Reinforced Plastics
  • Strain Gages
  • Surface Roughness
  • Tensile Strength
  • Test Methods

Readers

  • Reinforced Composite Materials
  • Software Engineering