RESEARCH AND DEVELOPMENT OF TITANIUM ROCKET MOTOR CASE

Abstract

On the basis of limited data (notched and sustained notched tensile strengths) on a full scale 40-in.-diam cylinder, a H content of 240 ppm had no detrimental effect at room temperature on flow-turned material aged to the 180, 000 psi yield strength level. TIG welding by an improved copper-fixturing technique produces more uniform weld bead geometry, substantially less weld porosity but no significant improvement in tensile ductility or fracture toughness as compared with steel fixturing. The failure stress for TIGwelded material was inversely proportional to the numerical incidence of porosity, regardless of the weld technique. Limited data indicated that electron beam welds are less susceptible than TIG welds to crack initiation and growth at weld porosity. Closed-die press forging of subscale 14-in.-diam and full scale 40- in.-diam domes at 1850 F with the reductions employed and using the present die configuration produced low tensile ductility after aging to the 180,000 psi yield strength level.

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Document Details

Document Type
Technical Report
Publication Date
Jan 31, 1962
Accession Number
AD0274334

Entities

People

  • Robert P. Brody
  • W.e. Hilfrich

Organizations

  • Pratt & Whitney

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Crystal Structure
  • Cyclic Tests
  • Fabrication
  • Heat Treatment
  • Jet Propulsion
  • Manufacturing
  • Materials
  • Mechanical Properties
  • Mechanical Working
  • Military Research
  • Munitions
  • Rocket Engines
  • Tensile Properties
  • Tensile Strength
  • Test And Evaluation
  • Test Methods

Fields of Study

  • Materials science

Readers

  • Mechanical Engineering/Mechanics of Materials.
  • Metallurgy

Technology Areas

  • Directed Energy
  • Microelectronics
  • Microelectronics - Microelectromechanical Systems