Evaluation of Polyimide/Glass Fiber Composites for Construction of Light Weight Pressure Vessels for Cryogenic Propellants.

Abstract

The application of polyimide resin as a matrix for glass filament-wound thin metal-lined pressure vessels was studied over a temperature range of -320 to 600 degrees F. Keramid 601 polyimide was found to perform quite well over the entire range of temperature. Hoop stress values of 425 ksi were determined at 75 degrees F which is equivalent to epoxy resin in similar structures. At -320 and 600 degrees F, 125 and 80% of this strength was retained. Thermal ageing at 500 degrees F for up to 50 hours was studied with severe reduction in strength, but there is evidence that this reduction could be improved. Another polyimide resin studied was P10PA which was found to have processing characteristics inappropriate for filament-winding. NOL ring tensile and shear data was determined from both resins with S-glass. Pressure vessel design, fabrication and test procedures are described in detail. (MM)

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Document Details

Document Type
Technical Report
Publication Date
Sep 01, 1973
Accession Number
ADA306161

Entities

People

  • I. Petker
  • M. Segimoto

Tags

Communities of Interest

  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Air Force
  • Composite Materials
  • Fabrication
  • Material Degradation Processes
  • Materials
  • Materials Laboratories
  • Materials Processing
  • Materials Science
  • Materials Testing
  • Measurement
  • Mechanical Properties
  • Mechanical Working
  • Mechanics
  • Modulus Of Elasticity
  • Stress Strain Relations
  • Tensile Strength
  • Test And Evaluation

Fields of Study

  • Materials science

Readers

  • Mechanical Engineering/Mechanics of Materials.
  • Reinforced Composite Materials