Design buckling curves for gun launched rockets
Abstract
An investigation of elastic buckling of gun-launched motor cases is considered. The SATANS finite difference computer program was used for the analysis. Comparative results from other buckling models were obtained to verify the results. The results are summarized in a set of design curves and show that for the proposed design parameters, the elastic behavior is exceeded before buckling can occur. (Author)
Rights
This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.NPS Report Number
NPS-59ZC73081ARelated items
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