THE FIBERGLASS MOTOR CASE IN THE POLARIS PROGRAM

Abstract

A comparison between the apparent practical limits of the usable tensile strength-density ratio for steels, Ti alloys, and glass-fiberreinforced plastic rocket-motor cases showed that the plastic motor case offers considerable advantages in weight and cost. Filament winding of fiberglass-reinforced motor cases produced greater simplicity and flexibility of tooling and fabrication techniques and shorter lead time than metal working. Theoretical and practical limitations on the strength of glass-reinforced materials in terms of flaws or defects are usually the result of fabrication, processing, handling, and storage. Methods for controlling these flaws are being evaluated. Failure of glass-reinforced plastic structures was partly caused by crazing and cracking of the resin binder. Shrinkage stresses in the resin were an important contributor to this process. A substantial increase in the performance of fiberglass motor cases in the near future appears possible if a study of defects and shrinkage stresses is included. (Author)

Document Details

Document Type
Technical Report
Publication Date
Sep 19, 1961
Accession Number
AD0264759

Entities

People

  • Herbert J Bernstein
  • J.a. Kies

Organizations

  • United States Naval Research Laboratory

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Cooperation
  • Fabrication
  • Fiberglass
  • Fibers
  • Filaments
  • Lead Time
  • Material Forming Processes
  • Materials
  • Materials Processing
  • Mechanical Working
  • Resilience
  • Rocket Engines
  • Rockets
  • Tensile Strength

Fields of Study

  • Materials science

Readers

  • Reinforced Composite Materials
  • Rocket Propulsion.