Accession Number : ADA310567
Title : Investigation of Thin Films as Floating Liners for Fiber-Glass Cryogenic Propellant Tanks.
Descriptive Note : Technical note,
Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION CLEVELAND OH LEWIS RESEARCH CEN TER
Personal Author(s) : Frischmuth, Robert W., Jr
PDF Url : ADA310567
Report Date : JAN 1966
Pagination or Media Count : 29
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.
Descriptors : *FIBERGLASS, *PROPELLANT TANKS, *REINFORCED PLASTICS, STRESS STRAIN RELATIONS, FILAMENT WOUND CONSTRUCTION, STRUCTURAL ANALYSIS, CRACKING(FRACTURING), FIBER REINFORCED COMPOSITES, THIN FILMS, HIGH PRESSURE, RUPTURE, LININGS, ALUMINUM, POLYMERIC FILMS, TENSION, PRESSURIZATION, LIQUID HYDROGEN, WEIGHT REDUCTION, LIQUID ROCKET PROPELLANTS, THERMAL STRESSES, TETRAFLUOROETHYLENE RESINS, CRYOGENIC PROPELLANTS, LAMINATED PLASTICS, BURSTING STRENGTH, TANK LINERS, POLYETHYLENE TEREPHTHALATE, STRUCTURAL INTEGRITY.
Subject Categories : Plastics
Liquid Rocket Propellants
Distribution Statement : APPROVED FOR PUBLIC RELEASE