Effects of closo-icosahedral periodoborane salts on hypergolic reactions of 70% H2O2 with energetic ionic liquids
A number of energetic ionic liquids (EILs) have been reported as promising hydrazine-replacement fuels for hypergolic rocket propulsion. However, most of these EILs were ignited using corrosive and hazardous concentrated fuming nitric acid. Very significant efforts were recently made to utilize “roc...
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creator | Chinnam, Ajay Kumar Petrutik, Natan Wang, Kangcai Shlomovich, Avital Shamis, Olga Tov, Daniel Shem Sućeska, Muhamed Qi-Long, Yan Dobrovetsky, Roman Gozin, Michael |
description | A number of energetic ionic liquids (EILs) have been reported as promising hydrazine-replacement fuels for hypergolic rocket propulsion. However, most of these EILs were ignited using corrosive and hazardous concentrated fuming nitric acid. Very significant efforts were recently made to utilize “rocket grade” highly concentrated H2O2 (>90%) as a “green” alternative to fuming nitric acid and N2O4 oxidizers. Although “rocket grade” H2O2 is more challenging to use and less safe for storage than commercially available H2O2 (70%), the latter is not considered as a viable oxidizer for hypergolic propulsion. In this work, we focused on the development of novel iodine-rich promoters, capable of initiating hypergolic ignition reactions between a typical EIL fuel – 3-ethyl-1-methyl-1H-imidazol-3-ium cyanotrihydroborate – and H2O2. Among the prepared and evaluated promoters, the top performing [FcCH2NEtMe2+]2[B12I122−] compound 5 showed ignition delay times of 45 ms in the reaction of the tested EIL with H2O2 (70%) and 17 ms with H2O2 (95%). We believe that these findings provide a platform for the development and utilization of commercially available H2O2 as a potential “green” oxidizer for rocket propulsion. |
doi_str_mv | 10.1039/c8ta03780a |
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However, most of these EILs were ignited using corrosive and hazardous concentrated fuming nitric acid. Very significant efforts were recently made to utilize “rocket grade” highly concentrated H2O2 (>90%) as a “green” alternative to fuming nitric acid and N2O4 oxidizers. Although “rocket grade” H2O2 is more challenging to use and less safe for storage than commercially available H2O2 (70%), the latter is not considered as a viable oxidizer for hypergolic propulsion. In this work, we focused on the development of novel iodine-rich promoters, capable of initiating hypergolic ignition reactions between a typical EIL fuel – 3-ethyl-1-methyl-1H-imidazol-3-ium cyanotrihydroborate – and H2O2. Among the prepared and evaluated promoters, the top performing [FcCH2NEtMe2+]2[B12I122−] compound 5 showed ignition delay times of 45 ms in the reaction of the tested EIL with H2O2 (70%) and 17 ms with H2O2 (95%). We believe that these findings provide a platform for the development and utilization of commercially available H2O2 as a potential “green” oxidizer for rocket propulsion.</description><identifier>ISSN: 2050-7488</identifier><identifier>EISSN: 2050-7496</identifier><identifier>DOI: 10.1039/c8ta03780a</identifier><language>eng</language><publisher>Cambridge: Royal Society of Chemistry</publisher><subject>Crystallography ; Delay time ; Hydrazine ; Hydrazines ; Hydrogen peroxide ; Icosahedral phase ; Ignition ; Iodine ; Ionic liquids ; Nitric acid ; Nitrogen tetroxide ; Oxidizing agents ; Promoters ; Rocket propulsion ; Rockets ; Salts</subject><ispartof>Journal of materials chemistry. 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A, Materials for energy and sustainability</title><description>A number of energetic ionic liquids (EILs) have been reported as promising hydrazine-replacement fuels for hypergolic rocket propulsion. However, most of these EILs were ignited using corrosive and hazardous concentrated fuming nitric acid. Very significant efforts were recently made to utilize “rocket grade” highly concentrated H2O2 (>90%) as a “green” alternative to fuming nitric acid and N2O4 oxidizers. Although “rocket grade” H2O2 is more challenging to use and less safe for storage than commercially available H2O2 (70%), the latter is not considered as a viable oxidizer for hypergolic propulsion. In this work, we focused on the development of novel iodine-rich promoters, capable of initiating hypergolic ignition reactions between a typical EIL fuel – 3-ethyl-1-methyl-1H-imidazol-3-ium cyanotrihydroborate – and H2O2. Among the prepared and evaluated promoters, the top performing [FcCH2NEtMe2+]2[B12I122−] compound 5 showed ignition delay times of 45 ms in the reaction of the tested EIL with H2O2 (70%) and 17 ms with H2O2 (95%). We believe that these findings provide a platform for the development and utilization of commercially available H2O2 as a potential “green” oxidizer for rocket propulsion.</description><subject>Crystallography</subject><subject>Delay time</subject><subject>Hydrazine</subject><subject>Hydrazines</subject><subject>Hydrogen peroxide</subject><subject>Icosahedral phase</subject><subject>Ignition</subject><subject>Iodine</subject><subject>Ionic liquids</subject><subject>Nitric acid</subject><subject>Nitrogen tetroxide</subject><subject>Oxidizing agents</subject><subject>Promoters</subject><subject>Rocket propulsion</subject><subject>Rockets</subject><subject>Salts</subject><issn>2050-7488</issn><issn>2050-7496</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2018</creationdate><recordtype>article</recordtype><recordid>eNo9jk9LAzEQxYMoWGovfoKAeFydTLKb5CilWqHQi55LNsm2Kcum3WQRv73xD85h3sD78d4QcsvggQHXj1ZlA1wqMBdkhlBDJYVuLv9vpa7JIqUjlFEAjdYzcl51nbc50dhR28cUq2BjMgfvRtPTkx9DdLGNoxk8Tab_Bgd6-CzGPvbB0tEbm0McfgIk3NM1bpF-hHygfiiQzwUqftl9OE_BpRty1Zk--cWfzsn78-ptua4225fX5dOm2iNCrph3otMomULJuRMNaNl6hEao8rBrsQYloNbCI28lds5IbZlnFiSyxgg-J3e_uacxnief8u4Yp3EolTtkKDjjoDX_Ah6DW_4</recordid><startdate>2018</startdate><enddate>2018</enddate><creator>Chinnam, Ajay Kumar</creator><creator>Petrutik, Natan</creator><creator>Wang, Kangcai</creator><creator>Shlomovich, Avital</creator><creator>Shamis, Olga</creator><creator>Tov, Daniel Shem</creator><creator>Sućeska, Muhamed</creator><creator>Qi-Long, Yan</creator><creator>Dobrovetsky, Roman</creator><creator>Gozin, Michael</creator><general>Royal Society of Chemistry</general><scope>7SP</scope><scope>7SR</scope><scope>7ST</scope><scope>7U5</scope><scope>8BQ</scope><scope>8FD</scope><scope>C1K</scope><scope>JG9</scope><scope>L7M</scope><scope>SOI</scope></search><sort><creationdate>2018</creationdate><title>Effects of closo-icosahedral periodoborane salts on hypergolic reactions of 70% H2O2 with energetic ionic liquids</title><author>Chinnam, Ajay Kumar ; Petrutik, Natan ; Wang, Kangcai ; Shlomovich, Avital ; Shamis, Olga ; Tov, Daniel Shem ; Sućeska, Muhamed ; Qi-Long, Yan ; Dobrovetsky, Roman ; Gozin, Michael</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-g220t-1ed4f927182733d46097be20648fecdb250840594e23b72fda79c1e1c07216a43</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2018</creationdate><topic>Crystallography</topic><topic>Delay time</topic><topic>Hydrazine</topic><topic>Hydrazines</topic><topic>Hydrogen peroxide</topic><topic>Icosahedral phase</topic><topic>Ignition</topic><topic>Iodine</topic><topic>Ionic liquids</topic><topic>Nitric acid</topic><topic>Nitrogen tetroxide</topic><topic>Oxidizing agents</topic><topic>Promoters</topic><topic>Rocket propulsion</topic><topic>Rockets</topic><topic>Salts</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Chinnam, Ajay Kumar</creatorcontrib><creatorcontrib>Petrutik, Natan</creatorcontrib><creatorcontrib>Wang, Kangcai</creatorcontrib><creatorcontrib>Shlomovich, Avital</creatorcontrib><creatorcontrib>Shamis, Olga</creatorcontrib><creatorcontrib>Tov, Daniel Shem</creatorcontrib><creatorcontrib>Sućeska, Muhamed</creatorcontrib><creatorcontrib>Qi-Long, Yan</creatorcontrib><creatorcontrib>Dobrovetsky, Roman</creatorcontrib><creatorcontrib>Gozin, Michael</creatorcontrib><collection>Electronics & Communications Abstracts</collection><collection>Engineered Materials Abstracts</collection><collection>Environment Abstracts</collection><collection>Solid State and Superconductivity Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Environmental Sciences and Pollution Management</collection><collection>Materials Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Environment Abstracts</collection><jtitle>Journal of materials chemistry. A, Materials for energy and sustainability</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Chinnam, Ajay Kumar</au><au>Petrutik, Natan</au><au>Wang, Kangcai</au><au>Shlomovich, Avital</au><au>Shamis, Olga</au><au>Tov, Daniel Shem</au><au>Sućeska, Muhamed</au><au>Qi-Long, Yan</au><au>Dobrovetsky, Roman</au><au>Gozin, Michael</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Effects of closo-icosahedral periodoborane salts on hypergolic reactions of 70% H2O2 with energetic ionic liquids</atitle><jtitle>Journal of materials chemistry. A, Materials for energy and sustainability</jtitle><date>2018</date><risdate>2018</risdate><volume>6</volume><issue>41</issue><spage>19989</spage><epage>19997</epage><pages>19989-19997</pages><issn>2050-7488</issn><eissn>2050-7496</eissn><abstract>A number of energetic ionic liquids (EILs) have been reported as promising hydrazine-replacement fuels for hypergolic rocket propulsion. However, most of these EILs were ignited using corrosive and hazardous concentrated fuming nitric acid. Very significant efforts were recently made to utilize “rocket grade” highly concentrated H2O2 (>90%) as a “green” alternative to fuming nitric acid and N2O4 oxidizers. Although “rocket grade” H2O2 is more challenging to use and less safe for storage than commercially available H2O2 (70%), the latter is not considered as a viable oxidizer for hypergolic propulsion. In this work, we focused on the development of novel iodine-rich promoters, capable of initiating hypergolic ignition reactions between a typical EIL fuel – 3-ethyl-1-methyl-1H-imidazol-3-ium cyanotrihydroborate – and H2O2. Among the prepared and evaluated promoters, the top performing [FcCH2NEtMe2+]2[B12I122−] compound 5 showed ignition delay times of 45 ms in the reaction of the tested EIL with H2O2 (70%) and 17 ms with H2O2 (95%). We believe that these findings provide a platform for the development and utilization of commercially available H2O2 as a potential “green” oxidizer for rocket propulsion.</abstract><cop>Cambridge</cop><pub>Royal Society of Chemistry</pub><doi>10.1039/c8ta03780a</doi><tpages>9</tpages></addata></record> |
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subjects | Crystallography Delay time Hydrazine Hydrazines Hydrogen peroxide Icosahedral phase Ignition Iodine Ionic liquids Nitric acid Nitrogen tetroxide Oxidizing agents Promoters Rocket propulsion Rockets Salts |
title | Effects of closo-icosahedral periodoborane salts on hypergolic reactions of 70% H2O2 with energetic ionic liquids |
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