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dc.contributor.authorSalinas, David
dc.contributor.authorBall, Robert E.
dc.dateInterim Report for Period July 1973-September 1973
dc.date.accessioned2013-02-27T23:38:03Z
dc.date.available2013-02-27T23:38:03Z
dc.date.issued1974-03-22
dc.identifier.urihttps://hdl.handle.net/10945/29484
dc.description.abstractAn investigation was undertaken to determine the radial pressure due to the slumping propellant in a gun-launched rocket motor case subject to high axial g loading during launch. Using a Rayleigh- Ritz formulation an approximate solution was obtained.en_US
dc.description.sponsorshipPrepared for: Commander, Naval Weapons Center, China Lake, California 93555en_US
dc.description.urihttp://archive.org/details/radialpressureon00sali
dc.language.isoen_US
dc.publisherMonterey, California. Naval Postgraduate Schoolen_US
dc.rightsThis 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.lcshALGORITHMS.en_US
dc.titleRadial pressure on a gun launched motor case due to slumping propellanten_US
dc.typeTechnical Reporten_US
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.subject.authorPropellanten_US
dc.subject.authorGun- launched rocketen_US
dc.subject.authorStress analysisen_US
dc.identifier.npsreportNPS-59Zc74031


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