RESEARCH AND DEVELOPMENT OF TITANIUM ROCKET MOTOR CASE

Abstract

Sustained-load notched strength of cold-rolled, aged sheet (H content of 70 ppm) at the 180,0 0 psi yield strength level is lower than that of 200 ppm H content sheet. The pronounced aging response at 900 F of press-forged material with 0.10 to 0.20% oxygen was reaffirmed. Multiplepass TIG welding on U- and V-type joints produced fine gains and superior ductility. Good tensile properties resulted from open-die press forging, and closed-die press forging of 14-in diameter domes. Closed-die hammer-forged pancakes exhibited nonuniform tensile properties after aging at 800 or 900 F. Subscale 14-in. diameter rings roll-forged at 1800 to 20 0 F were satisfactory in tensile ductility and flowturnability. Residual stresses of 165,000 psi average and 200,000 psi maximum were measured in the circumferential direction in as-flow-turned 9.4-in-diam. cylinders; stress relief treatment at 900 to 950 f gave satisfactory relief.

Document Details

Document Type
Technical Report
Publication Date
Jul 31, 1961
Accession Number
AD0264570

Entities

People

  • Robert P. Brody
  • William E. Helfrich

Organizations

  • Pratt & Whitney

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Diameters
  • Ductility
  • Forging
  • Gas Tungsten Arc Welding
  • Joints
  • Materials
  • Mechanical Properties
  • Nonuniform
  • Physical Properties
  • Press Forging
  • Residual Stress
  • Residuals
  • Rocket Engines
  • Stresses
  • Tensile Properties
  • Yield Strength

Fields of Study

  • Materials science

Readers

  • Metallurgy