Accession Number : AD0674603
Title : TANKAGE MATERIALS IN LIQUID PROPELLANTS.
Descriptive Note : Final rept. 1 Jun 67-1 Jun 68,
Corporate Author : DOUGLAS AIRCRAFT CO INC NEWPORT BEACH CALIF ASTROPOWER LAB
Personal Author(s) : Toy,S. M. ; Bell,L. E. ; English,W. D. ; Tiner,N. A.
Report Date : JUL 1968
Pagination or Media Count : 120
Abstract : The report discusses the work conducted on Air Force Contract F33615-67-C-1718 concerning the study of engineering behavior of tankage materials in liquid propellants. A survey of literature about the type and form of impact data required by tank designers was made. Modified ABMA open-cup impact tests on Al 2014-T6 and Ti-6Al-4V (ELI) in the oxidizers N2O4, ClF5, and LF2 were conducted. (Author)
Descriptors : (*PROPELLANT TANKS, LIQUID ROCKET PROPELLANTS), (*MATERIALS, PROPELLANT TANKS), COMPATIBILITY, IMPACT TESTS, LITHIUM FLUORIDES, LIQUID ROCKET OXIDIZERS, STRESSES, STRAIN(MECHANICS), ELASTIC PROPERTIES, FRICTION, YIELD POINT, ALUMINUM ALLOYS, TITANIUM ALLOYS, STAINLESS STEEL, MATHEMATICAL ANALYSIS, TEST METHODS
Subject Categories : Metallurgy and Metallography
Liquid Propellant Rocket Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE