Design buckling curves for gun launched rockets

dc.contributor.author	Salinas, David
dc.contributor.author	Ball, Robert E.
dc.date	8/24/1973
dc.date.accessioned	2013-02-27T23:36:40Z
dc.date.available	2013-02-27T23:36:40Z
dc.date.issued	1973-08-24
dc.identifier.uri	https://hdl.handle.net/10945/29242
dc.description.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)	en_US
dc.description.sponsorship	Naval Weapons Center, China Lake, California, Work Request No. 2-3128	en_US
dc.description.uri	http://archive.org/details/designbucklingcu00sali
dc.format.extent	NA	en_US
dc.language.iso	en_US
dc.publisher	Monterey, California. Naval Postgraduate School	en_US
dc.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.	en_US
dc.subject.lcsh	PROGRAMMING LANGUAGES (ELECTRONIC COMPUTERS)	en_US
dc.title	Design buckling curves for gun launched rockets	en_US
dc.type	Technical Report	en_US
dc.contributor.corporate	Naval Postgraduate School (U.S.)
dc.description.recognition	NA	en_US
dc.identifier.oclc	NA
dc.identifier.npsreport	NPS-59ZC73081A

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