Burning Characteristics of the HMX/CL‐20/AP/Polyvinyltetrazole Binder/Al Solid Propellants Loaded with Nanometals
The paper investigated the effect of metal nanopowders additive on the combustion properties of HMX/CL‐20/AP/polyvinyltetrazole binder/Al propellants. Using thermal analysis, the authors described the effect of aluminum, boron, zinc, nickel, copper, and molybdenum and identified the combustion in a...
Gespeichert in:
| Veröffentlicht in: | Propellants, explosives, pyrotechnics explosives, pyrotechnics, 2019-02, Vol.44 (2), p.217-223 |
|---|---|
| Hauptverfasser: | , , , , , , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 223 |
|---|---|
| container_issue | 2 |
| container_start_page | 217 |
| container_title | Propellants, explosives, pyrotechnics |
| container_volume | 44 |
| creator | Sergienko, Alexey V. Popenko, Elena M. Slyusarsky, Konstantin V. Larionov, Kirill B. Dzidziguri, Ella L. Kondratyeva, Elena S. Gromov, Alexander A. |
| description | The paper investigated the effect of metal nanopowders additive on the combustion properties of HMX/CL‐20/AP/polyvinyltetrazole binder/Al propellants. Using thermal analysis, the authors described the effect of aluminum, boron, zinc, nickel, copper, and molybdenum and identified the combustion in a pressure range from 4 to 10 MPa with a pressure step of 1 MPa. No significant correlation between the oxidation properties of the n‐Me powders and the combustion properties of propellants was discovered. An addition of nanopowders caused an increase in the propellant burning rate by approximately 30 % for n‐Al, n‐B, n‐Ni, and n‐Mo independent from the pressure values. An addition of n‐Cu resulted in a burning rate increase by a factor of 4.9 due to coppers’ probable catalytic activity during interaction with nitroesters and cyclic nitramines in a solid phase. n‐Zn additive increased the propellant burning rate by factors 2.3 and 3.6 at 4 and 10 MPa, respectively, due to catalytic activity of zinc in a gaseous phase. |
| doi_str_mv | 10.1002/prep.201800204 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2175807527</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2175807527</sourcerecordid><originalsourceid>FETCH-LOGICAL-c3174-50836584b65ee46cc447fa32abc08a3883bc6e50e08cf9ffd67a3347879a1cea3</originalsourceid><addsrcrecordid>eNqFkMtOwzAQRS0EEuWxZW2JdZtxnMTuslS8pAIRD4ld5DoTamTiYLugsuIT-Ea-hKAiWLK6M9I9M7qXkAMGIwaQJp3HbpQCk_0C2QYZsDxlwwyk2CQDEP3MGcu3yU4IjwA9AmxAwtHSt6Z9oNOF8kpH9CZEowN1DY0LpGcX98l09vn-kUIyKZPS2dWLaVc2YvTqzVmkR6at0ScTS2-cNTUtvevQWtXGQGdO1VjTVxMX9FK17gmjsmGPbDW94P6P7pK7k-Pb6dlwdnV6Pp3MhpozkQ1zkLzIZTYvcsSs0DrLRKN4quYapOJS8rkuMAcEqZtx09SFUJxnQoqxYhoV3yWH67udd89LDLF6dH3a_mWVMpFLEHkqetdo7dLeheCxqTpvnpRfVQyq72Kr72Kr32J7YLwGXo3F1T_uqrw-Lv_YL8Gkfhs</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2175807527</pqid></control><display><type>article</type><title>Burning Characteristics of the HMX/CL‐20/AP/Polyvinyltetrazole Binder/Al Solid Propellants Loaded with Nanometals</title><source>Wiley Online Library Journals Frontfile Complete</source><creator>Sergienko, Alexey V. ; Popenko, Elena M. ; Slyusarsky, Konstantin V. ; Larionov, Kirill B. ; Dzidziguri, Ella L. ; Kondratyeva, Elena S. ; Gromov, Alexander A.</creator><creatorcontrib>Sergienko, Alexey V. ; Popenko, Elena M. ; Slyusarsky, Konstantin V. ; Larionov, Kirill B. ; Dzidziguri, Ella L. ; Kondratyeva, Elena S. ; Gromov, Alexander A.</creatorcontrib><description>The paper investigated the effect of metal nanopowders additive on the combustion properties of HMX/CL‐20/AP/polyvinyltetrazole binder/Al propellants. Using thermal analysis, the authors described the effect of aluminum, boron, zinc, nickel, copper, and molybdenum and identified the combustion in a pressure range from 4 to 10 MPa with a pressure step of 1 MPa. No significant correlation between the oxidation properties of the n‐Me powders and the combustion properties of propellants was discovered. An addition of nanopowders caused an increase in the propellant burning rate by approximately 30 % for n‐Al, n‐B, n‐Ni, and n‐Mo independent from the pressure values. An addition of n‐Cu resulted in a burning rate increase by a factor of 4.9 due to coppers’ probable catalytic activity during interaction with nitroesters and cyclic nitramines in a solid phase. n‐Zn additive increased the propellant burning rate by factors 2.3 and 3.6 at 4 and 10 MPa, respectively, due to catalytic activity of zinc in a gaseous phase.</description><identifier>ISSN: 0721-3115</identifier><identifier>EISSN: 1521-4087</identifier><identifier>DOI: 10.1002/prep.201800204</identifier><language>eng</language><publisher>Weinheim: Wiley Subscription Services, Inc</publisher><subject>aluminized solid propellant ; Aluminum ; Boron ; Burning rate ; Catalysis ; Catalytic activity ; Combustion ; Copper ; HMX ; Molybdenum ; nanometal ; Nickel ; non-isothermal oxidation ; Oxidation ; Properties (attributes) ; Solid phases ; Solid propellants ; Thermal analysis ; Zinc</subject><ispartof>Propellants, explosives, pyrotechnics, 2019-02, Vol.44 (2), p.217-223</ispartof><rights>2019 Wiley‐VCH Verlag GmbH & Co. KGaA, Weinheim</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c3174-50836584b65ee46cc447fa32abc08a3883bc6e50e08cf9ffd67a3347879a1cea3</citedby><cites>FETCH-LOGICAL-c3174-50836584b65ee46cc447fa32abc08a3883bc6e50e08cf9ffd67a3347879a1cea3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://onlinelibrary.wiley.com/doi/pdf/10.1002%2Fprep.201800204$$EPDF$$P50$$Gwiley$$H</linktopdf><linktohtml>$$Uhttps://onlinelibrary.wiley.com/doi/full/10.1002%2Fprep.201800204$$EHTML$$P50$$Gwiley$$H</linktohtml><link.rule.ids>314,776,780,1411,27901,27902,45550,45551</link.rule.ids></links><search><creatorcontrib>Sergienko, Alexey V.</creatorcontrib><creatorcontrib>Popenko, Elena M.</creatorcontrib><creatorcontrib>Slyusarsky, Konstantin V.</creatorcontrib><creatorcontrib>Larionov, Kirill B.</creatorcontrib><creatorcontrib>Dzidziguri, Ella L.</creatorcontrib><creatorcontrib>Kondratyeva, Elena S.</creatorcontrib><creatorcontrib>Gromov, Alexander A.</creatorcontrib><title>Burning Characteristics of the HMX/CL‐20/AP/Polyvinyltetrazole Binder/Al Solid Propellants Loaded with Nanometals</title><title>Propellants, explosives, pyrotechnics</title><description>The paper investigated the effect of metal nanopowders additive on the combustion properties of HMX/CL‐20/AP/polyvinyltetrazole binder/Al propellants. Using thermal analysis, the authors described the effect of aluminum, boron, zinc, nickel, copper, and molybdenum and identified the combustion in a pressure range from 4 to 10 MPa with a pressure step of 1 MPa. No significant correlation between the oxidation properties of the n‐Me powders and the combustion properties of propellants was discovered. An addition of nanopowders caused an increase in the propellant burning rate by approximately 30 % for n‐Al, n‐B, n‐Ni, and n‐Mo independent from the pressure values. An addition of n‐Cu resulted in a burning rate increase by a factor of 4.9 due to coppers’ probable catalytic activity during interaction with nitroesters and cyclic nitramines in a solid phase. n‐Zn additive increased the propellant burning rate by factors 2.3 and 3.6 at 4 and 10 MPa, respectively, due to catalytic activity of zinc in a gaseous phase.</description><subject>aluminized solid propellant</subject><subject>Aluminum</subject><subject>Boron</subject><subject>Burning rate</subject><subject>Catalysis</subject><subject>Catalytic activity</subject><subject>Combustion</subject><subject>Copper</subject><subject>HMX</subject><subject>Molybdenum</subject><subject>nanometal</subject><subject>Nickel</subject><subject>non-isothermal oxidation</subject><subject>Oxidation</subject><subject>Properties (attributes)</subject><subject>Solid phases</subject><subject>Solid propellants</subject><subject>Thermal analysis</subject><subject>Zinc</subject><issn>0721-3115</issn><issn>1521-4087</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><recordid>eNqFkMtOwzAQRS0EEuWxZW2JdZtxnMTuslS8pAIRD4ld5DoTamTiYLugsuIT-Ea-hKAiWLK6M9I9M7qXkAMGIwaQJp3HbpQCk_0C2QYZsDxlwwyk2CQDEP3MGcu3yU4IjwA9AmxAwtHSt6Z9oNOF8kpH9CZEowN1DY0LpGcX98l09vn-kUIyKZPS2dWLaVc2YvTqzVmkR6at0ScTS2-cNTUtvevQWtXGQGdO1VjTVxMX9FK17gmjsmGPbDW94P6P7pK7k-Pb6dlwdnV6Pp3MhpozkQ1zkLzIZTYvcsSs0DrLRKN4quYapOJS8rkuMAcEqZtx09SFUJxnQoqxYhoV3yWH67udd89LDLF6dH3a_mWVMpFLEHkqetdo7dLeheCxqTpvnpRfVQyq72Kr72Kr32J7YLwGXo3F1T_uqrw-Lv_YL8Gkfhs</recordid><startdate>201902</startdate><enddate>201902</enddate><creator>Sergienko, Alexey V.</creator><creator>Popenko, Elena M.</creator><creator>Slyusarsky, Konstantin V.</creator><creator>Larionov, Kirill B.</creator><creator>Dzidziguri, Ella L.</creator><creator>Kondratyeva, Elena S.</creator><creator>Gromov, Alexander A.</creator><general>Wiley Subscription Services, Inc</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>201902</creationdate><title>Burning Characteristics of the HMX/CL‐20/AP/Polyvinyltetrazole Binder/Al Solid Propellants Loaded with Nanometals</title><author>Sergienko, Alexey V. ; Popenko, Elena M. ; Slyusarsky, Konstantin V. ; Larionov, Kirill B. ; Dzidziguri, Ella L. ; Kondratyeva, Elena S. ; Gromov, Alexander A.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c3174-50836584b65ee46cc447fa32abc08a3883bc6e50e08cf9ffd67a3347879a1cea3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2019</creationdate><topic>aluminized solid propellant</topic><topic>Aluminum</topic><topic>Boron</topic><topic>Burning rate</topic><topic>Catalysis</topic><topic>Catalytic activity</topic><topic>Combustion</topic><topic>Copper</topic><topic>HMX</topic><topic>Molybdenum</topic><topic>nanometal</topic><topic>Nickel</topic><topic>non-isothermal oxidation</topic><topic>Oxidation</topic><topic>Properties (attributes)</topic><topic>Solid phases</topic><topic>Solid propellants</topic><topic>Thermal analysis</topic><topic>Zinc</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Sergienko, Alexey V.</creatorcontrib><creatorcontrib>Popenko, Elena M.</creatorcontrib><creatorcontrib>Slyusarsky, Konstantin V.</creatorcontrib><creatorcontrib>Larionov, Kirill B.</creatorcontrib><creatorcontrib>Dzidziguri, Ella L.</creatorcontrib><creatorcontrib>Kondratyeva, Elena S.</creatorcontrib><creatorcontrib>Gromov, Alexander A.</creatorcontrib><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>Propellants, explosives, pyrotechnics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Sergienko, Alexey V.</au><au>Popenko, Elena M.</au><au>Slyusarsky, Konstantin V.</au><au>Larionov, Kirill B.</au><au>Dzidziguri, Ella L.</au><au>Kondratyeva, Elena S.</au><au>Gromov, Alexander A.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Burning Characteristics of the HMX/CL‐20/AP/Polyvinyltetrazole Binder/Al Solid Propellants Loaded with Nanometals</atitle><jtitle>Propellants, explosives, pyrotechnics</jtitle><date>2019-02</date><risdate>2019</risdate><volume>44</volume><issue>2</issue><spage>217</spage><epage>223</epage><pages>217-223</pages><issn>0721-3115</issn><eissn>1521-4087</eissn><abstract>The paper investigated the effect of metal nanopowders additive on the combustion properties of HMX/CL‐20/AP/polyvinyltetrazole binder/Al propellants. Using thermal analysis, the authors described the effect of aluminum, boron, zinc, nickel, copper, and molybdenum and identified the combustion in a pressure range from 4 to 10 MPa with a pressure step of 1 MPa. No significant correlation between the oxidation properties of the n‐Me powders and the combustion properties of propellants was discovered. An addition of nanopowders caused an increase in the propellant burning rate by approximately 30 % for n‐Al, n‐B, n‐Ni, and n‐Mo independent from the pressure values. An addition of n‐Cu resulted in a burning rate increase by a factor of 4.9 due to coppers’ probable catalytic activity during interaction with nitroesters and cyclic nitramines in a solid phase. n‐Zn additive increased the propellant burning rate by factors 2.3 and 3.6 at 4 and 10 MPa, respectively, due to catalytic activity of zinc in a gaseous phase.</abstract><cop>Weinheim</cop><pub>Wiley Subscription Services, Inc</pub><doi>10.1002/prep.201800204</doi><tpages>7</tpages></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 0721-3115 |
| ispartof | Propellants, explosives, pyrotechnics, 2019-02, Vol.44 (2), p.217-223 |
| issn | 0721-3115 1521-4087 |
| language | eng |
| recordid | cdi_proquest_journals_2175807527 |
| source | Wiley Online Library Journals Frontfile Complete |
| subjects | aluminized solid propellant Aluminum Boron Burning rate Catalysis Catalytic activity Combustion Copper HMX Molybdenum nanometal Nickel non-isothermal oxidation Oxidation Properties (attributes) Solid phases Solid propellants Thermal analysis Zinc |
| title | Burning Characteristics of the HMX/CL‐20/AP/Polyvinyltetrazole Binder/Al Solid Propellants Loaded with Nanometals |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-12T19%3A10%3A38IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Burning%20Characteristics%20of%20the%20HMX/CL%E2%80%9020/AP/Polyvinyltetrazole%20Binder/Al%20Solid%20Propellants%20Loaded%20with%20Nanometals&rft.jtitle=Propellants,%20explosives,%20pyrotechnics&rft.au=Sergienko,%20Alexey%20V.&rft.date=2019-02&rft.volume=44&rft.issue=2&rft.spage=217&rft.epage=223&rft.pages=217-223&rft.issn=0721-3115&rft.eissn=1521-4087&rft_id=info:doi/10.1002/prep.201800204&rft_dat=%3Cproquest_cross%3E2175807527%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2175807527&rft_id=info:pmid/&rfr_iscdi=true |