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首页> 外文期刊>Journal of Energetic Materials >Formulation and Comparative Study of Rheological Properties of Loaded and Unloaded Ethanol-Based Gel Propellants
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Formulation and Comparative Study of Rheological Properties of Loaded and Unloaded Ethanol-Based Gel Propellants

机译:负载型和卸载型乙醇基凝胶推进剂的流变性能的制定与比较研究

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The current trend in the area of highly energetic storable liquid rocket propellant research is to develop environmentally friendly gelled/metallized systems and to explore the feasibility of their application in rocket engines. The idea stems from the fact that the conversion of a conventional liquid propellant to a gelled state and its subsequent metallization has the potential to significantly enhance the performance and density-specific impulse. The gelation of liquid fuels could be induced at a critical gellant concentration of as low as 8wt% for the pure ethanol case and as low as 4 and 6wt% for metallized ethanol depending on the metal type. Furthermore, the gel formed should be thixotropic. Metallized gels using 20wt% Al and B metal powders could also be formulated. These metallized (Al and B) ethanol gel systems showed a reduction in the critical gellant concentration depending on the degree of metallization. The rheological properties of metallized and nonmetallized ethanol gels using methyl cellulose (MC) as a gelling agent at different ambient temperatures (283.15, 293.15, 303.15, 313.15, and 323.15K) were experimentally investigated in this study. The gel fuels were rheologically characterized using a rheometer at shear rates ranging from 1 to 12s(-1) and 1 to 1,000s(-1). Metallized and nonmetallized ethanol gels were found to be thixotropic in nature. The apparent viscosity and yield stress (for shear rate range 1 to 12s(-1)) of gels were observed to significantly decrease at higher ambient temperatures and as the gellant and metal particle concentrations decreased. The thixotropic behavior was found to be a strong function of the Al and B metal particle concentration for all test temperatures at shear rate ranges from 1 to 12s(-1) and 1 to 1,000s(-1). It was also a function of the MC concentration at a shear rate range of 1 to 1,000s(-1).
机译:高能储存液体火箭推进剂研究领域的当前趋势是开发环保的胶凝/金属化系统,并探索其在火箭发动机中应用的可行性。该思想源于以下事实:常规的液体推进剂转化为胶凝状态,随后进行的金属化处理具有显着增强性能和密度比冲量的潜力。取决于金属类型,在纯乙醇情况下,可在低至8wt%的临界胶凝剂浓度下诱导液体燃料的胶凝,而对于金属化乙醇,则可在低至4wt%和6wt%的临界胶凝剂浓度下诱导胶凝。此外,形成的凝胶应该是触变的。也可以配制使用20wt%Al和B金属粉末的金属化凝胶。这些金属化的(Al和B)乙醇凝胶体系显示出取决于金属化程度的临界胶凝剂浓度的降低。在本研究中,通过实验研究了使用甲基纤维素(MC)作为胶凝剂的金属化和非金属化乙醇凝胶在不同环境温度(283.15、293.15、303.15、313.15和323.15K)下的流变特性。使用流变仪在1至12s(-1)和1至1,000s(-1)的剪切速率下对凝胶燃料进行流变学表征。发现金属化和非金属化的乙醇凝胶本质上具有触变性。观察到凝胶的表观粘度和屈服应力(剪切速率范围为1至12s(-1))在较高的环境温度下以及随着胶凝剂和金属颗粒浓度的降低而显着降低。在剪切速率范围为1至12s(-1)和1至1,000s(-1)的所有测试温度下,触变行为是Al和B金属颗粒浓度的强函数。它也是剪切速率范围为1至1,000s(-1)时MC浓度的函数。

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