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dc.contributor.authorNetzer, David Willis
dc.contributor.authorAbraham, Michael
dc.contributor.authorKlahr, Owen Allen
dc.contributor.authorGerhard, Robert Ross
dc.date1 July 1972 - 1 Jan 197^
dc.date.accessioned2013-03-07T21:53:06Z
dc.date.available2013-03-07T21:53:06Z
dc.date.issued1974-03
dc.identifier.urihttp://hdl.handle.net/10945/29937
dc.description.abstractNonmetallized double-base and composite propellant, metallized composite propellant, and ammonium perchlorate (AP)/binder sandwich combustion were studied in standard and high acceleration environments Experimental techniques used were high speed motion pictures, twocolor schlieren, laser schlieren, and centrifuge mounted combustion bombs. It was found for double-base propellant that the temperature increased continuously from the surface into the visible flame.en_US
dc.description.sponsorshipNaval Ordnance Systems Commanden_US
dc.description.urihttp://archive.org/details/investigationofso00abra
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. As such, it is in the public domain, and under the provisions of Title 17, United States Code, Section 105, may not be copyrighted.en_US
dc.subject.lcshHEAT--TRANSMISSION--INSTRUMENTS.en_US
dc.titleAn investigation of solid propellant combustion in standard and high acceleration environmentsen_US
dc.typeTechnical Reporten_US
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.subject.authorSolid Propellanten_US
dc.subject.authorCombustionen_US
dc.subject.authorAccelerationen_US
dc.description.recognitionNAen_US
dc.identifier.oclcNA
dc.identifier.npsreportNPS-57Nt-7U031


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