REPORT ON SPECIAL MEETING TO DISCUSS NONDESTRUCTIVE TESTS FOR FILAMENT WOUND FIBERGLASS MOTOR CASES ON 24-25 JANUARY 1963 AT AEROJET-GENERAL CORPORATION, SACRAMENTO

Abstract

Various non-destructive test procedures (ultrasonics, microwaves, X rays, corona discharge, and ion scattering) for detecting flaws, voids, defects delamination and fracture in fiberglass wound composite rocket motor cases are reviewed and discussed. (LS-PL).

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1963
Accession Number
AD0296094

Entities

People

  • Stephen D. Hart

Organizations

  • United States Naval Research Laboratory

Tags

Communities of Interest

  • Advanced Electronics
  • Weapons Technologies

DTIC Thesaurus Topics

  • Composite Materials
  • Corporations
  • Delamination
  • Destructive Tests
  • Detectors
  • Fast Neutrons
  • Fiberglass
  • Frequency
  • Government Procurement
  • High Voltage
  • Inspection
  • Materials
  • Measurement
  • Rocket Engines
  • Scattering
  • Standing Waves
  • X Rays

Fields of Study

  • Physics

Readers

  • Reinforced Composite Materials
  • Solar Physics
  • Structural Health Monitoring of Composite Structures.