Design and Development of Storable Propellant Tanks

Abstract

The report describes the results of a program to design, evaluate and deliver full scale, flight-weight positive expulsion propellant tank systems for inclusion in the storability program. The cylindrical design is comprised of a maraging steel (250 grade) outer shell inside of which is installed an all- aluminum rolling diaphragm positive expulsion system. All materials of construction are compatible with N2O4 for long term storage. A test phase was conducted, consisting of a successful hot gas expulsion test to demonstrate the design under operational environments, followed by fabrication and delivery of units for inclusion in the storability program.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1969
Accession Number
AD0854131

Entities

People

  • Thomas J. O'grady

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Alloys
  • Assembly
  • Fabrication
  • Hot Gases
  • Liquid Propellants
  • Manufacturing
  • Maraging Steels
  • Materials
  • Materials Laboratories
  • Measurement
  • Metals
  • Positive Expulsion
  • Propellants
  • Surface Tension
  • Tensile Strength
  • Test Methods

Fields of Study

  • Physics

Readers

  • Metallurgy
  • Rocket Propulsion.
  • Software Engineering