THE ENVIRONMENT CREATED BY AN OPEN-AIR SOLID ROCKET PROPELLANT FIRE
A 91 kg (200 lb m ) block of aluminized solid rocket propellant was burned in open air to simulate an accidental propellant fire. A suite of remote optical instruments measured the temperature and radiative properties of the plume. Solid molybdenum calorimeters provided data for heat flux estimates....
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| Veröffentlicht in: | Combustion science and technology 2007-05, Vol.179 (5), p.1003-1027 |
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| container_title | Combustion science and technology |
| container_volume | 179 |
| creator | HUNTER, L. W. CHANG, Y. OGUZ, H. N. WILKERSON, J. T. LENNON, A. M. CAIN, R. P. CARKHUFF, B. G. THOMAS, M. E. WALTS, S. C. MITCHELL, C. A. BLODGETT, D. W. TERRY, D. H. |
| description | A 91 kg (200 lb
m
) block of aluminized solid rocket propellant was burned in open air to simulate an accidental propellant fire. A suite of remote optical instruments measured the temperature and radiative properties of the plume. Solid molybdenum calorimeters provided data for heat flux estimates. Various refractory oxide and metallic witness samples placed in the fire provided temperature benchmarks and insight into how such samples may be dispersed by the fire. A thermochemical analysis assessed the overall energy balance. The results indicate that temperatures reached 3000±100 K and heat fluxes reached 200±80 W/cm
2
under the propellant, which burned for 120 s, creating a severe environment. |
| doi_str_mv | 10.1080/00102200600910833 |
| format | Article |
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m
) block of aluminized solid rocket propellant was burned in open air to simulate an accidental propellant fire. A suite of remote optical instruments measured the temperature and radiative properties of the plume. Solid molybdenum calorimeters provided data for heat flux estimates. Various refractory oxide and metallic witness samples placed in the fire provided temperature benchmarks and insight into how such samples may be dispersed by the fire. A thermochemical analysis assessed the overall energy balance. The results indicate that temperatures reached 3000±100 K and heat fluxes reached 200±80 W/cm
2
under the propellant, which burned for 120 s, creating a severe environment.</description><identifier>ISSN: 0010-2202</identifier><identifier>EISSN: 1563-521X</identifier><identifier>DOI: 10.1080/00102200600910833</identifier><identifier>CODEN: CBSTB9</identifier><language>eng</language><publisher>London: Taylor & Francis Group</publisher><subject>Applied sciences ; Combustion. Flame ; Energy ; Energy. Thermal use of fuels ; Exact sciences and technology ; Fire ; Heat transfer ; Miscellaneous ; Radiation ; Solid propellant ; Theoretical studies. Data and constants. Metering</subject><ispartof>Combustion science and technology, 2007-05, Vol.179 (5), p.1003-1027</ispartof><rights>Copyright Taylor & Francis Group, LLC 2007</rights><rights>2007 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c407t-db00ca875b684f5a9b51bcff02ce35c3ff938d084678382d5b7c781b60e06c103</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://www.tandfonline.com/doi/pdf/10.1080/00102200600910833$$EPDF$$P50$$Ginformaworld$$H</linktopdf><linktohtml>$$Uhttps://www.tandfonline.com/doi/full/10.1080/00102200600910833$$EHTML$$P50$$Ginformaworld$$H</linktohtml><link.rule.ids>314,776,780,27901,27902,59620,60409</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=18790868$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>HUNTER, L. W.</creatorcontrib><creatorcontrib>CHANG, Y.</creatorcontrib><creatorcontrib>OGUZ, H. N.</creatorcontrib><creatorcontrib>WILKERSON, J. T.</creatorcontrib><creatorcontrib>LENNON, A. M.</creatorcontrib><creatorcontrib>CAIN, R. P.</creatorcontrib><creatorcontrib>CARKHUFF, B. G.</creatorcontrib><creatorcontrib>THOMAS, M. E.</creatorcontrib><creatorcontrib>WALTS, S. C.</creatorcontrib><creatorcontrib>MITCHELL, C. A.</creatorcontrib><creatorcontrib>BLODGETT, D. W.</creatorcontrib><creatorcontrib>TERRY, D. H.</creatorcontrib><title>THE ENVIRONMENT CREATED BY AN OPEN-AIR SOLID ROCKET PROPELLANT FIRE</title><title>Combustion science and technology</title><description>A 91 kg (200 lb
m
) block of aluminized solid rocket propellant was burned in open air to simulate an accidental propellant fire. A suite of remote optical instruments measured the temperature and radiative properties of the plume. Solid molybdenum calorimeters provided data for heat flux estimates. Various refractory oxide and metallic witness samples placed in the fire provided temperature benchmarks and insight into how such samples may be dispersed by the fire. A thermochemical analysis assessed the overall energy balance. The results indicate that temperatures reached 3000±100 K and heat fluxes reached 200±80 W/cm
2
under the propellant, which burned for 120 s, creating a severe environment.</description><subject>Applied sciences</subject><subject>Combustion. Flame</subject><subject>Energy</subject><subject>Energy. Thermal use of fuels</subject><subject>Exact sciences and technology</subject><subject>Fire</subject><subject>Heat transfer</subject><subject>Miscellaneous</subject><subject>Radiation</subject><subject>Solid propellant</subject><subject>Theoretical studies. Data and constants. Metering</subject><issn>0010-2202</issn><issn>1563-521X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2007</creationdate><recordtype>article</recordtype><recordid>eNqFkMFOhDAQhhujievqA3jjojd0SrdQEi-I1SUiGESjJ1IKTTDsoi1G9-3tZjUejPE0mZnv-zMZhA4xnGBgcAqAwfMAfIDQDgjZQhNMfeJSDz9uo8l671rA20V7xjzblhAPT1BczrnDs4ekyLMbnpVOXPCo5BfO-ZMTZU5-yzM3SgrnLk-TC6fI42teOreFnadpZPHLpOD7aEeJ3rQHX3WK7i95Gc_dNL9K4ih15QyC0W1qAClYQGufzRQVYU1xLZUCT7aESqJUSFgDbOYHjDCvoXUgA4ZrH1rwJQYyRceb3Bc9vL61ZqwWnZFt34tlO7yZygvDGYWQWhBvQKkHY3SrqhfdLYReVRiq9buqX--yztFXuDBS9EqLpezMj8iCEJjPLBdsuG6pBr0Q74Pum2oUq37Q39Kv9Gr8GK159q9J_j7wEwmdh04</recordid><startdate>200705</startdate><enddate>200705</enddate><creator>HUNTER, L. W.</creator><creator>CHANG, Y.</creator><creator>OGUZ, H. N.</creator><creator>WILKERSON, J. T.</creator><creator>LENNON, A. M.</creator><creator>CAIN, R. P.</creator><creator>CARKHUFF, B. G.</creator><creator>THOMAS, M. E.</creator><creator>WALTS, S. C.</creator><creator>MITCHELL, C. A.</creator><creator>BLODGETT, D. W.</creator><creator>TERRY, D. H.</creator><general>Taylor & Francis Group</general><general>Taylor & Francis</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>200705</creationdate><title>THE ENVIRONMENT CREATED BY AN OPEN-AIR SOLID ROCKET PROPELLANT FIRE</title><author>HUNTER, L. W. ; CHANG, Y. ; OGUZ, H. N. ; WILKERSON, J. T. ; LENNON, A. M. ; CAIN, R. P. ; CARKHUFF, B. G. ; THOMAS, M. E. ; WALTS, S. C. ; MITCHELL, C. A. ; BLODGETT, D. W. ; TERRY, D. H.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c407t-db00ca875b684f5a9b51bcff02ce35c3ff938d084678382d5b7c781b60e06c103</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2007</creationdate><topic>Applied sciences</topic><topic>Combustion. Flame</topic><topic>Energy</topic><topic>Energy. Thermal use of fuels</topic><topic>Exact sciences and technology</topic><topic>Fire</topic><topic>Heat transfer</topic><topic>Miscellaneous</topic><topic>Radiation</topic><topic>Solid propellant</topic><topic>Theoretical studies. Data and constants. Metering</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>HUNTER, L. W.</creatorcontrib><creatorcontrib>CHANG, Y.</creatorcontrib><creatorcontrib>OGUZ, H. N.</creatorcontrib><creatorcontrib>WILKERSON, J. T.</creatorcontrib><creatorcontrib>LENNON, A. M.</creatorcontrib><creatorcontrib>CAIN, R. P.</creatorcontrib><creatorcontrib>CARKHUFF, B. G.</creatorcontrib><creatorcontrib>THOMAS, M. E.</creatorcontrib><creatorcontrib>WALTS, S. C.</creatorcontrib><creatorcontrib>MITCHELL, C. A.</creatorcontrib><creatorcontrib>BLODGETT, D. W.</creatorcontrib><creatorcontrib>TERRY, D. H.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Combustion science and technology</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>HUNTER, L. W.</au><au>CHANG, Y.</au><au>OGUZ, H. N.</au><au>WILKERSON, J. T.</au><au>LENNON, A. M.</au><au>CAIN, R. P.</au><au>CARKHUFF, B. G.</au><au>THOMAS, M. E.</au><au>WALTS, S. C.</au><au>MITCHELL, C. A.</au><au>BLODGETT, D. W.</au><au>TERRY, D. H.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>THE ENVIRONMENT CREATED BY AN OPEN-AIR SOLID ROCKET PROPELLANT FIRE</atitle><jtitle>Combustion science and technology</jtitle><date>2007-05</date><risdate>2007</risdate><volume>179</volume><issue>5</issue><spage>1003</spage><epage>1027</epage><pages>1003-1027</pages><issn>0010-2202</issn><eissn>1563-521X</eissn><coden>CBSTB9</coden><abstract>A 91 kg (200 lb
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2
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| language | eng |
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| source | Taylor & Francis Journals Complete |
| subjects | Applied sciences Combustion. Flame Energy Energy. Thermal use of fuels Exact sciences and technology Fire Heat transfer Miscellaneous Radiation Solid propellant Theoretical studies. Data and constants. Metering |
| title | THE ENVIRONMENT CREATED BY AN OPEN-AIR SOLID ROCKET PROPELLANT FIRE |
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