Accession Number : AD0284206
Title : THERMAL GRAIN STRUCTURAL ANALYSIS
Corporate Author : LOCKHEED PROPULSION CO REDLANDS CALIF
Personal Author(s) : SEWARD,A.L.
Report Date : 14 SEP 1962
Pagination or Media Count : 1
Abstract : Methods for determining temperature distributions for cylindrical grains under various types of surface temperature variations were developed for the subsequent viscoelastic transient thermal stress analysis. These methods were verified by experiments performed on cylindrical grains with thermocouples cast in place. The viscoelastic thermal stress problem has been reduced for computer programming. Results of uniaxial thermal cycling experiments are presented. The effects of temperature on viscoelastic behavior have been determined experimentally and experimental results of failure tests on case-bonded grains are included.
Descriptors : *PROPELLANT GRAINS, BONDING, COMPUTERS, CONFIGURATION, COOLING, ELASTIC PROPERTIES, EQUATIONS, MATHEMATICAL ANALYSIS, MATHEMATICAL PREDICTION, ROCKET ENGINES, SEGMENTED ROCKET ENGINES, SOLID ROCKET PROPELLANTS, STRESSES, SURFACE TEMPERATURE, TEMPERATURE, TEST METHODS, THEORY, VISCOSITY
Distribution Statement : APPROVED FOR PUBLIC RELEASE