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Generating Plateau Burning Segments for Composite Solid Rocket Propellants

机译:为复合固体火箭推进剂产生高原燃烧段

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Abstract >Plateau burning is a highly desired phenomenon for composite solid rocket propellants. Three composite propellant compositions were prepared in an attempt to generate plateau burning segments. In these compositions the curative type was changed along with controlling the coarse to fine ratio of the oxidizer particles. The prepared compositions were extensively tested at one‐MPa segments from 1 to 14?MPa through strand burner technique. The results showed that depriving the combustion process from the thermal energy causes the plateau to exist. The thermal depriving was achieved through controlling the spacing of coarse and fine particle of the oxidizer, to reduce the intensity of their combustion flame, and through employing binders that possess high activation energy for the first decomposition stage. These findings were proven through the appearance of bi‐plateau segments for the first time for one of the employed isocyanates. </abstract> </span> <span class="z_kbtn z_kbtnclass hoverxs" style="display: none;">展开▼</span> </div> <div class="translation abstracttxt"> <span class="zhankaihshouqi fivelineshidden" id="abstract"> <span>机译:</span><Abstract Type =“Main”XML:Lang =“en”> <标题类型=“main”>抽象</ title> >平台燃烧是复合固体火箭推进剂的高度期望的现象。制备三种复合推进剂组合物以试图产生高原燃烧段。在这些组合物中,疗效随着控制氧化剂颗粒的粗比率而改变。通过股线燃烧器技术在1至14℃的单MPa段以3至14℃,在一个MPa区段中进行广泛测试制备的组合物。结果表明,从热能剥夺燃烧过程会导致高原存在。通过控制氧化剂的粗糙和细颗粒的间隔来实现热剥离,以降低其燃烧火焰的强度,并通过采用具有高活化能量的粘合剂来实现第一分解阶段的粘合剂。这些发现是通过Bi-Plateau段的出现第一次用于使用的异氰酸酯。</ p> </摘要> </span> <span class="z_kbtn z_kbtnclass hoverxs" style="display: none;">展开▼</span> </div> </div> <div class="record"> <h2 class="all_title" id="enpatent33" >著录项</h2> <ul> <li> <span class="lefttit">来源</span> <div style="width: 86%;vertical-align: text-top;display: inline-block;"> <a href='/journal-foreign-29946/'>《Propellants, Explosives, Pyrotechnics》</a> <b style="margin: 0 2px;">|</b><span>2020年第1期</span><b style="margin: 0 2px;">|</b><span>共6页</span> </div> </li> <li> <div class="author"> <span class="lefttit">作者</span> <p id="fAuthorthree" class="threelineshidden zhankaihshouqi"> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=El‐Basuony Sameh A.&option=202" target="_blank" rel="nofollow">El‐Basuony Sameh A.;</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Sadek Mohamed A.&option=202" target="_blank" rel="nofollow">Sadek Mohamed A.;</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Wafy Tamer Z.&option=202" target="_blank" rel="nofollow">Wafy Tamer Z.;</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Mostafa Hosam E.&option=202" target="_blank" rel="nofollow">Mostafa Hosam E.;</a> </p> <span class="z_kbtnclass z_kbtnclassall hoverxs" id="zkzz" style="display: none;">展开▼</span> </div> </li> <li> <div style="display: flex;"> <span class="lefttit">作者单位</span> <div style="position: relative;margin-left: 3px;max-width: 639px;"> <div class="threelineshidden zhankaihshouqi" id="fOrgthree"> <p>Military Technical College11766 Kobry El-Kobba Cairo Egypt;</p> <p>Department of Chemical EngineeringThe British University in Egypt11837 El-Sherouk City Cairo Egypt;</p> <p>Military Technical College11766 Kobry El-Kobba Cairo Egypt;</p> <p>Military Technical College11766 Kobry El-Kobba Cairo Egypt;</p> </div> <span class="z_kbtnclass z_kbtnclassall hoverxs" id="zhdw" style="display: none;">展开▼</span> </div> </div> </li> <li > <span class="lefttit">收录信息</span> <span style="width: 86%;vertical-align: text-top;display: inline-block;"></span> </li> <li> <span class="lefttit">原文格式</span> <span>PDF</span> </li> <li> <span class="lefttit">正文语种</span> <span>eng</span> </li> <li> <span class="lefttit">中图分类</span> <span><a href="https://www.zhangqiaokeyan.com/clc/1837.html" title="爆炸物工业、火柴工业">爆炸物工业、火柴工业;</a></span> </li> <li class="antistop"> <span class="lefttit">关键词</span> <p style="width: 86%;vertical-align: text-top;"> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=composite propellants&option=203" rel="nofollow">composite propellants;</a> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=plateau burning&option=203" rel="nofollow">plateau burning;</a> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=HTPB&option=203" rel="nofollow">HTPB;</a> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=ammonium perchlorate&option=203" rel="nofollow">ammonium perchlorate;</a> </p> <div class="translation"> 机译:复合推进剂;高原燃烧;HTPB;高氯酸铵铵; </div> </li> </ul> </div> </div> <div class="literature cardcommon"> <div class="similarity "> <h3 class="all_title" id="enpatent66">相似文献</h3> <div class="similaritytab clearfix"> <ul> <li class="active" >外文文献</li> <li >中文文献</li> <li >专利</li> </ul> </div> <div class="similarity_details"> <ul > <li> <div> <b>1. </b><a class="enjiyixqcontent" href="/journal-foreign-detail/0704024626179.html">Generating Plateau Burning Segments for Composite Solid Rocket Propellants</a> <b>[J]</b> . <span> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=El‐Basuony Sameh A.&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">El‐Basuony Sameh A.,</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Sadek Mohamed A.&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">Sadek Mohamed A.,</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Wafy Tamer Z.&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">Wafy Tamer Z.,</a> <a href="/journal-foreign-29946/" target="_blank" rel="nofollow" class="tuijian_authcolor">Propellants, Explosives, Pyrotechnics .</a> <span>2020</span><span>,第1期</span> </span> </div> <p class="zwjiyix translation" style="max-width: initial;height: auto;word-break: break-all;white-space: initial;text-overflow: initial;overflow: initial;"> <span>机译:为复合固体火箭推进剂产生高原燃烧段</span> </p> </li> <li> <div> <b>2. </b><a class="enjiyixqcontent" href="/journal-foreign-detail/0704019403070.html">Burning-rate enhancement of a high-energy rocket composite solid propellant based on ferrocene-grafted hydroxyl-terminated polybutadiene binder</a> <b>[J]</b> . <span> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Saravanakumar D.&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">Saravanakumar D.,</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Sengottuvelan N.&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">Sengottuvelan N.,</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Narayanan V.&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">Narayanan V.,</a> <a href="/journal-foreign-33581/" target="_blank" rel="nofollow" class="tuijian_authcolor">Journal of Applied Polymer Science .</a> <span>2011</span><span>,第5期</span> </span> </div> <p class="zwjiyix translation" style="max-width: initial;height: auto;word-break: break-all;white-space: initial;text-overflow: initial;overflow: initial;"> <span>机译:基于二茂铁接枝的羟基封端的聚丁二烯粘合剂的高能火箭复合固体推进剂的燃烧速率提高</span> </p> </li> <li> <div> <b>3. </b><a class="enjiyixqcontent" href="/academic-journal-foreign_journal-propulsion-power_thesis/02041643779.html">Nano Additives and Plateau Burning Rates of Ammonium-Perchlorate-Based Composite Solid Propellants</a> <b>[J]</b> . <span> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Matthew A. 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solid propellants and homogeneous solid propellants for rocket systems</a> <b>[P]</b> . <span> 外国专利: <!-- --> CZ20150180A3 </span> <span> . 2016-10-26</span> </div> <p class="zwjiyix translation" style="max-width: initial;height: auto;word-break: break-all;white-space: initial;text-overflow: initial;overflow: initial;"> <span>机译:均质固体推进剂和火箭系统中均质固体推进剂中的燃烧改性剂 </span> </p> </li> <li> <div> <b>5. </b><a class="enjiyixqcontent" href="/patent-detail/06130488291858.html">Positive displacement control system for controlling the flow of gases within a solid-propellant rocket motor to regulate the burning rate of the solid propellant</a> <b>[P]</b> . <span> 外国专利: <!-- 美国专利: --> US3418811A </span> <span> . 1968-12-31</span> </div> <p class="zwjiyix translation" style="max-width: initial;height: auto;word-break: break-all;white-space: initial;text-overflow: initial;overflow: initial;"> <span>机译:正排量控制系统,用于控制固体推进剂火箭发动机内的气体流量,以调节固体推进剂的燃烧速率 </span> </p> </li> </ul> </div> </div> </div> <div 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