'T-END CLOSURE STUDY FOR POLARIS A-3 ROCKET MOTOR CASE

Abstract

Design studies were begun of the aft dome section of the Polaris A-3 rocket motor case with the following objectives: (1) analyze the magnitude of stresses and stress distribution around the port openings; (2) determine structural requirements for port reinforcement and design optimum reinforcement for the stress pattern; (3) investigate use of a more ductile type of Al alloy for aft cluster fitting; (4) analyze shape of aft cluster and recommend shape which will reduce bending stress under pressure to a minimum; and (5) develop optimum flexible bond between Al cluster fitting and fiber glass chamber. Theoretical computations were made of stresses at port openings. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jul 11, 1961
Accession Number
AD0262530

Entities

People

  • H. W. Stevenson
  • R. A. Harrington

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Bending Stress
  • Computations
  • Pressure Distribution
  • Rocket Engines
  • Rockets
  • Stresses

Readers

  • Combustion and Flow Dynamics.
  • Quantum Chemistry
  • Reinforced Composite Materials