AFT-END CLOSURE STUDY FOR POLARIS A-3 ROCKET MOTOR CASE

Abstract

Testing of shear test specimens was continued to determine the optimum adhesive bond between the aluminum cluster fitting and the fiberglass chamber. Testing of double-lap specimens is reported. Fabrication and testing of subscale chambers was continued. Four additional chambers were also tested. (Au hor)

Document Details

Document Type
Technical Report
Publication Date
Dec 30, 1961
Accession Number
AD0269042

Entities

People

  • H.w. Stevenson
  • R.a. Harrington

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Adhesives
  • Aluminum
  • Fabrication
  • Fiberglass
  • Materials
  • Materials Testing
  • Rocket Engines
  • Rockets
  • Shear Tests

Readers

  • Materials Science and Engineering.
  • Rocket Propulsion.
  • Structural Health Monitoring of Composite Structures.