Accession Number : AD0781381
Title : Minuteman STV Stress Analysis and Testing.
Descriptive Note : Final rept. 1 Dec 71-2 Jul 73,
Corporate Author : THIOKOL CORP BRIGHAM CITY UTAH WASATCH DIV
Personal Author(s) : Danieu,D. J. ; Ruggles,V. L.
Report Date : JUN 1974
Pagination or Media Count : 37
Abstract : The report presents a theoretical stress analysis of OOAMA/RPL Motor S/N 0012257. The analysis involved predicting stresses induced by temperature cycling, temperature shock, and pressurization. The results reported represent a major step in the use of instrumented motors to verify the accuracy of modulus dependent predictions of rocket motor grain structural behavior. (Author)
Descriptors : *Surface to surface missiles, *Solid propellant rocket engines, *Solid rocket propellants, Stresses, Stress testing, Thermal shock, Rocket propellant grains, Viscoelasticity
Subject Categories : Solid Propellant Rocket Engines
Solid Rocket Propellants
Distribution Statement : APPROVED FOR PUBLIC RELEASE