MALFUNCTION INVESTIGATION OF ROCKET, PRACTICE, 3.5-INCH: M29A2 AND ROCKET, SMOKE, 3.5-INCH: WP, M30 (RUPTURED MOTOR BODIES),

Abstract

Malfunction investigations were made of practice rockets and smoke rockets. The rockets malfunctioned because the igniter functioned with a force sufficient to split the motor from end to end, partially disrupted the tail assembly and split the rear barrel assembly from the launcher. It was determined that these malfunctions were caused by the presence of a lap at the outer surface and of intermediate transformation products in the microstructure which acted as a focal point for stress concentration, reducing the effective cross-sectional area, and lowering the impact and tensile strength of the motor body; excessive nonmetallic inclusions in the steel being drawn into stringers in the tubing wall parallel to the axis; severe quenching after heat-treatment to meet required physical condition, and cracking at the nozzle mouth due to forging and heat-treating. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1963
Accession Number
AD0423409

Entities

People

  • John Mcpartland
  • Joseph V. Urodzinski

Organizations

  • Picatinny Arsenal

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Assembly
  • Heat Treatment
  • Inclusions
  • Launchers
  • Malfunctions
  • Microstructure
  • Quenching
  • Rockets
  • Smoke
  • Stress Concentration
  • Stresses
  • Tail Assemblies
  • Tensile Strength

Readers

  • Mathematics or Statistics
  • Metallurgy
  • Rocket Propulsion.