4C and 11D Failure Analysis of Helium Pressure Regulator (Fuel Tank) DWR. NO. 27-08217-3

Abstract

This test was conducted to analyze failures that occurred in the airborne pressurization system of missiles 4C and 11D. The objective of the test was to determine if heating of the motor section pressure/bleed line on the regulator would result in a condition similar to that which caused the failures.

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Document Details

Document Type
Technical Report
Publication Date
Aug 11, 1960
Accession Number
AD0842100

Entities

People

  • D. J. Melvin

Organizations

  • General Dynamics

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Airborne
  • Altitude
  • Astronautics
  • Battleships
  • Buildings And Structures
  • Electron Tube Heaters
  • Engineers
  • Export Controls
  • Failure Analysis
  • Fuel Tanks
  • Government (Foreign)
  • Governments
  • Pressure Regulators
  • Pressurization
  • Regulators
  • Research Facilities

Readers

  • Combustion and Flow Dynamics.
  • Materials Science