Accession Number : AD0805549

Title :   LIQUID ROCKET SYSTEM CONJUGATE STRUCTURE AND TANKAGE PROGRAM.

Descriptive Note : Quarterly progress rept. no. 5, 1 Sep-30 Nov 66,

Corporate Author : NORTH AMERICAN AVIATION INC LOS ANGELES CA LOS ANGELES DIV

Personal Author(s) : Conn, Charles E.

Report Date : JAN 1967

Pagination or Media Count : 62

Abstract : The objective of the Conjugate Structure and Tankage Program is to acquire design and test data that will demonstrate and verify the potential value of titanium 'Jaffee-metal' (sandwich structure material) in obtaining a higher strength-to-weight ratio and a higher stage mass fraction for liquid rocket system structures and tankage. The object of this procurement will be to provide the structure and tankage assembly fabricated from titanium 'Jaffee-metal' for use in future planned test and evaluation.

Descriptors :   (*PROPELLANT TANKS, LIQUID PROPELLANT ROCKET ENGINES), SANDWICH CONSTRUCTION, TITANIUM ALLOYS, SANDWICH PANELS, ALUMINUM ALLOYS, VANADIUM ALLOYS, ROLLING(METALLURGY), CONSTRUCTION, MANUFACTURING, TITANIUM, BONDING.

Subject Categories : Liquid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE