Accession Number : AD0436438


Title :   INVESTIGATION OF FILAMENT WINDING PATTERNS.


Descriptive Note : Bimonthly progress rept. no. 5, 24 Dec 6324 Feb 64.


Corporate Author : AEROJET-GENERAL CORP SACRAMENTO CALIF


Report Date : 27 Mar 1964


Pagination or Media Count : 13


Abstract : Progress is reported on a program conducted to increase the understanding of the interrelation between chamber winding patterns and chamber behavior. All of the ten units originally included in Phase I of this program were hydrostatically tested and the data analyzed. The design of the deformation-control-evaluation chamber for Phase II of the program was initiated on the basis of a developed orthotropic analytical approach modified to reflect the changes that occur in orthotropic properties with load. (Author)


Descriptors :   ROCKET ENGINE CASES , PRESSURE VESSELS , DEFORMATION , HYDROSTATIC PRESSURE , FAILURE(MECHANICS) , EXPERIMENTAL DATA


Distribution Statement : APPROVED FOR PUBLIC RELEASE