Automated Grain Design for Solid Propellant High Low Ballistic Systems
This report documents the use of a computer program written in Fortran IV for the generation of the geometry of solid propellant grains required of high-low propellant actuated devices to produce a specified output. Program input consists of the desired performance, propellant, and system parameters...
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| creator | DeStefano, Leonard A |
| description | This report documents the use of a computer program written in Fortran IV for the generation of the geometry of solid propellant grains required of high-low propellant actuated devices to produce a specified output. Program input consists of the desired performance, propellant, and system parameters; program output consists of the required dimensions of one-, three-, and seven-perforation propellant grains. The computer program, system equations, selected derivations, and comparison with an experimental test are presented. (Author) |
| format | Report |
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Program input consists of the desired performance, propellant, and system parameters; program output consists of the required dimensions of one-, three-, and seven-perforation propellant grains. The computer program, system equations, selected derivations, and comparison with an experimental test are presented. (Author)</description><language>eng</language><subject>BURNING RATE ; CARTRIDGES(PAD) ; COMBUSTION ; COMPUTER PROGRAMMING ; Computer Programming and Software ; COMPUTER PROGRAMS ; FLOW CHARTING ; INTERIOR BALLISTICS ; LEAST SQUARES METHOD ; ROCKET PROPELLANT GRAINS ; Solid Rocket Propellants ; SPECIFIC HEAT ; THERMAL ANALYSIS</subject><creationdate>1969</creationdate><rights>APPROVED FOR PUBLIC RELEASE</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,776,881,27544,27545</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/AD0864145$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>DeStefano, Leonard A</creatorcontrib><creatorcontrib>FRANKFORD ARSENAL PHILADELPHIA PA</creatorcontrib><title>Automated Grain Design for Solid Propellant High Low Ballistic Systems</title><description>This report documents the use of a computer program written in Fortran IV for the generation of the geometry of solid propellant grains required of high-low propellant actuated devices to produce a specified output. Program input consists of the desired performance, propellant, and system parameters; program output consists of the required dimensions of one-, three-, and seven-perforation propellant grains. The computer program, system equations, selected derivations, and comparison with an experimental test are presented. (Author)</description><subject>BURNING RATE</subject><subject>CARTRIDGES(PAD)</subject><subject>COMBUSTION</subject><subject>COMPUTER PROGRAMMING</subject><subject>Computer Programming and Software</subject><subject>COMPUTER PROGRAMS</subject><subject>FLOW CHARTING</subject><subject>INTERIOR BALLISTICS</subject><subject>LEAST SQUARES METHOD</subject><subject>ROCKET PROPELLANT GRAINS</subject><subject>Solid Rocket Propellants</subject><subject>SPECIFIC HEAT</subject><subject>THERMAL ANALYSIS</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1969</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZHBzLC3Jz00sSU1RcC9KzMxTcEktzkzPU0jLL1IIzs_JTFEIKMovSM3JScwrUfDITM9Q8MkvV3BKzMnJLC7JTFYIriwuSc0t5mFgTUvMKU7lhdLcDDJuriHOHropQEXxQJV5qSXxji4GFmYmhiamxgSkAdofL_I</recordid><startdate>196910</startdate><enddate>196910</enddate><creator>DeStefano, Leonard A</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>196910</creationdate><title>Automated Grain Design for Solid Propellant High Low Ballistic Systems</title><author>DeStefano, Leonard A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD08641453</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1969</creationdate><topic>BURNING RATE</topic><topic>CARTRIDGES(PAD)</topic><topic>COMBUSTION</topic><topic>COMPUTER PROGRAMMING</topic><topic>Computer Programming and Software</topic><topic>COMPUTER PROGRAMS</topic><topic>FLOW CHARTING</topic><topic>INTERIOR BALLISTICS</topic><topic>LEAST SQUARES METHOD</topic><topic>ROCKET PROPELLANT GRAINS</topic><topic>Solid Rocket Propellants</topic><topic>SPECIFIC HEAT</topic><topic>THERMAL ANALYSIS</topic><toplevel>online_resources</toplevel><creatorcontrib>DeStefano, Leonard A</creatorcontrib><creatorcontrib>FRANKFORD ARSENAL PHILADELPHIA PA</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>DeStefano, Leonard A</au><aucorp>FRANKFORD ARSENAL PHILADELPHIA PA</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Automated Grain Design for Solid Propellant High Low Ballistic Systems</btitle><date>1969-10</date><risdate>1969</risdate><abstract>This report documents the use of a computer program written in Fortran IV for the generation of the geometry of solid propellant grains required of high-low propellant actuated devices to produce a specified output. 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| language | eng |
| recordid | cdi_dtic_stinet_AD0864145 |
| source | DTIC Technical Reports |
| subjects | BURNING RATE CARTRIDGES(PAD) COMBUSTION COMPUTER PROGRAMMING Computer Programming and Software COMPUTER PROGRAMS FLOW CHARTING INTERIOR BALLISTICS LEAST SQUARES METHOD ROCKET PROPELLANT GRAINS Solid Rocket Propellants SPECIFIC HEAT THERMAL ANALYSIS |
| title | Automated Grain Design for Solid Propellant High Low Ballistic Systems |
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