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Development of Polyurethane-Based Solid Propellants Using Nanocomposite Materials
Mechanically‐activated nanocomposites (MANCs) of nano‐aluminum (nAl)/X (X=Cu, Ni, Zn, Mg, and graphite) were used as replacements for reference nAl powder and as catalytic ingredients in polyurethane (PU) propellants. The effects of their use on combustion heat, burning rate, and thermal decompositi...
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Published in: | Propellants, explosives, pyrotechnics explosives, pyrotechnics, 2016-04, Vol.41 (2), p.286-294 |
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cited_by | cdi_FETCH-LOGICAL-c3882-239afef45615f8c8830a357e3f1705de04fa068dfcaac593cc36797cbbfd32693 |
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cites | cdi_FETCH-LOGICAL-c3882-239afef45615f8c8830a357e3f1705de04fa068dfcaac593cc36797cbbfd32693 |
container_end_page | 294 |
container_issue | 2 |
container_start_page | 286 |
container_title | Propellants, explosives, pyrotechnics |
container_volume | 41 |
creator | Ahmed, The late Abd El-Shafey I. Ali, Amged A. El-Masry, Ahmed M. Tawfik, Sayed M. |
description | Mechanically‐activated nanocomposites (MANCs) of nano‐aluminum (nAl)/X (X=Cu, Ni, Zn, Mg, and graphite) were used as replacements for reference nAl powder and as catalytic ingredients in polyurethane (PU) propellants. The effects of their use on combustion heat, burning rate, and thermal decomposition were investigated. It was found that MANCs have catalytic effects and the modified propellants have enhanced the released heat, burning rate, and thermal decomposition properties. MANCs‐based propellants have improved the processing and the mechanical properties with acceptable safety aspects. They can be used for catalytic applications in solid propellants to improve their energetic, burning rate, and thermal decomposition characteristics. |
doi_str_mv | 10.1002/prep.201500182 |
format | article |
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The effects of their use on combustion heat, burning rate, and thermal decomposition were investigated. It was found that MANCs have catalytic effects and the modified propellants have enhanced the released heat, burning rate, and thermal decomposition properties. MANCs‐based propellants have improved the processing and the mechanical properties with acceptable safety aspects. 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They can be used for catalytic applications in solid propellants to improve their energetic, burning rate, and thermal decomposition characteristics.</description><subject>Burning rate</subject><subject>Catalysis</subject><subject>Catalysts</subject><subject>Combustion</subject><subject>Decomposition</subject><subject>Mechanically activated nanocomposites</subject><subject>Polyurethane propellant</subject><subject>Polyurethane resins</subject><subject>Propellants</subject><subject>Solid propellants</subject><subject>Thermal decomposition</subject><issn>0721-3115</issn><issn>1521-4087</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2016</creationdate><recordtype>article</recordtype><recordid>eNqFkElPwzAQRi0EEmW5co7EhUuKlzh2jiylIEoJmzhaxhlDShIHOwX67wkUIcSFw-ibw3uj0YfQDsFDgjHdbz20Q4oJx5hIuoIGhFMSJ1iKVTTAot8ZIXwdbYQw6xHczwBdHcMrVK6toekiZ6PcVYu5h-5JNxAf6gBFdOOqsohy71qoKt10IboLZfMYTXXjjKtbF8oOogvdgS91FbbQmu0Dtr9zE92djG6PTuPJ5fjs6GASGyYljSnLtAWb8JRwK42UDGvGBTBLBOYF4MRqnMrCGq0Nz5gxLBWZMA8PtmA0zdgm2lvebb17mUPoVF0G8_UiuHlQRGKJM05p2qO7f9CZm_um_04RIYlIE8aSnhouKeNdCB6san1Za79QBKvPhtVnw-qn4V7IlsJbWcHiH1rl16P8txsv3TJ08P7jav-sUsEEV_fTsaKSZOe3fKLu2Qc0ko7_</recordid><startdate>201604</startdate><enddate>201604</enddate><creator>Ahmed, The late Abd El-Shafey I.</creator><creator>Ali, Amged A.</creator><creator>El-Masry, Ahmed M.</creator><creator>Tawfik, Sayed M.</creator><general>WILEY-VCH Verlag</general><general>WILEY‐VCH Verlag</general><general>Wiley Subscription Services, Inc</general><scope>BSCLL</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope><scope>7QF</scope><scope>JG9</scope></search><sort><creationdate>201604</creationdate><title>Development of Polyurethane-Based Solid Propellants Using Nanocomposite Materials</title><author>Ahmed, The late Abd El-Shafey I. ; Ali, Amged A. ; El-Masry, Ahmed M. ; Tawfik, Sayed M.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c3882-239afef45615f8c8830a357e3f1705de04fa068dfcaac593cc36797cbbfd32693</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2016</creationdate><topic>Burning rate</topic><topic>Catalysis</topic><topic>Catalysts</topic><topic>Combustion</topic><topic>Decomposition</topic><topic>Mechanically activated nanocomposites</topic><topic>Polyurethane propellant</topic><topic>Polyurethane resins</topic><topic>Propellants</topic><topic>Solid propellants</topic><topic>Thermal decomposition</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Ahmed, The late Abd El-Shafey I.</creatorcontrib><creatorcontrib>Ali, Amged A.</creatorcontrib><creatorcontrib>El-Masry, Ahmed M.</creatorcontrib><creatorcontrib>Tawfik, Sayed M.</creatorcontrib><collection>Istex</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><collection>Aluminium Industry Abstracts</collection><collection>Materials Research Database</collection><jtitle>Propellants, explosives, pyrotechnics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Ahmed, The late Abd El-Shafey I.</au><au>Ali, Amged A.</au><au>El-Masry, Ahmed M.</au><au>Tawfik, Sayed M.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Development of Polyurethane-Based Solid Propellants Using Nanocomposite Materials</atitle><jtitle>Propellants, explosives, pyrotechnics</jtitle><addtitle>Propellants, Explosives, Pyrotechnics</addtitle><date>2016-04</date><risdate>2016</risdate><volume>41</volume><issue>2</issue><spage>286</spage><epage>294</epage><pages>286-294</pages><issn>0721-3115</issn><eissn>1521-4087</eissn><abstract>Mechanically‐activated nanocomposites (MANCs) of nano‐aluminum (nAl)/X (X=Cu, Ni, Zn, Mg, and graphite) were used as replacements for reference nAl powder and as catalytic ingredients in polyurethane (PU) propellants. The effects of their use on combustion heat, burning rate, and thermal decomposition were investigated. It was found that MANCs have catalytic effects and the modified propellants have enhanced the released heat, burning rate, and thermal decomposition properties. MANCs‐based propellants have improved the processing and the mechanical properties with acceptable safety aspects. They can be used for catalytic applications in solid propellants to improve their energetic, burning rate, and thermal decomposition characteristics.</abstract><cop>Weinheim</cop><pub>WILEY-VCH Verlag</pub><doi>10.1002/prep.201500182</doi><tpages>9</tpages></addata></record> |
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source | Wiley-Blackwell Read & Publish Collection |
subjects | Burning rate Catalysis Catalysts Combustion Decomposition Mechanically activated nanocomposites Polyurethane propellant Polyurethane resins Propellants Solid propellants Thermal decomposition |
title | Development of Polyurethane-Based Solid Propellants Using Nanocomposite Materials |
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