Investigation of Thin Films as Floating Liners for Fiber-Glass Cryogenic Propellant Tanks.

Abstract

The use of filament-wound fiber-glass liquid-hydrogen propellant tank structures should result in a considerable weight savings providing that a suitable internal liner can be developed. This report investigates the use of free-floating liners (not bonded to the inner surface of the filament-wound shell). A theoretical analysis and experimental study on laminated Mylar, Teflon, and aluminum-Mylar liners showed that upon tank pressurization at liquid-hydrogen temperatures, plastic liners fabricated to the internal dimensions of the filament-wound structure would fail in tension before the burst pressure of the filament-wound shell was approached.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1966
Accession Number
ADA310567

Entities

People

  • Robert W. Frischmuth Jr.

Organizations

  • Glenn Research Center

Tags

DTIC Thesaurus Topics

  • Aluminum
  • Cryogenic Propellants
  • Energetic Materials
  • Filaments
  • Films
  • Hydrogen
  • Liquid Hydrogen
  • Liquid Propellants
  • Liquid Rocket Propellants
  • Materials
  • Pressurization
  • Propellant Tanks
  • Propellants
  • Thin Films

Fields of Study

  • Physics

Readers

  • Reinforced Composite Materials
  • Rocket Propulsion.