DEVELOPMENT OF HIGH PERFORMANCE ROCKET MOTOR CASE

Abstract

Design drawings were completed for the 20 in. diameter test chamber in the development of a solid rocket motor case. Two alloys, Ti-13V11Cr-3Al alloy and 20% nickel steel having 1.7 Ti and 0.5 Al, were selected as the fabricating materials. Manufacturing of the cases was begun. Welding tests were continued.

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Document Details

Document Type
Technical Report
Publication Date
Dec 31, 1961
Accession Number
AD0271065

Entities

People

  • R.c. Dethloff

Tags

Communities of Interest

  • C4I
  • Energy and Power Technologies
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Alloys
  • Gas Tungsten Arc Welding
  • Hardness
  • Materials
  • Mechanical Properties
  • Mechanical Working
  • Military Research
  • Munitions
  • Nickel Alloys
  • Nickel Steels
  • Rocket Engines
  • Rockets
  • Standards
  • Stresses
  • Tensile Properties
  • Tensile Strength
  • Yield Strength

Fields of Study

  • Materials science

Readers

  • Logistics and Supply Chain Management.
  • Surface Engineering/Surface Coating Technology.