Evaluation Test of Liquid Oxygen Topping Line System Convair Drawing No. 27-21516,

Abstract

This report describes tests performed on topping lines. The object of this was to determine if the re-designed liquid oxygen topping line would meet missile requirements. The topping line assembly was subjected to the Proof Pressure, Vibration, and Burst Tests as outlined in the procedure. The operation satisfied all design requirements. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 27, 1961
Accession Number
AD0844180

Entities

People

  • C. A. Palosaari

Organizations

  • General Dynamics

Tags

DTIC Thesaurus Topics

  • Assembly
  • Cryogenic Propellants
  • Energetic Materials
  • Fabrication
  • Liquid Oxygen
  • Liquid Propellants
  • Liquid Rocket Propellants
  • Materials
  • Mechanical Waves
  • Motion
  • Test And Evaluation
  • Vibration

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