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Keywords liquid propellant;explode;shockwave;superpressure; 液体推进剂;爆炸;冲击波;超压;
Keywords liquid propellant;droplet combustion;microexplosion; 液体推进剂;液滴燃烧;微爆;
Keywords liquid propellant;leaking;cleaning and disinfecting; 液体推进剂;泄漏;洗消;
Keywords Liquid propellant;Unsymmetrical dimethylhydrazine;Potentiometry titration;Programme designation; 液体推进剂;偏二甲肼;电位滴定;程序设计;
Keywords liquid propellant;hydroxylammonium nitrate;hydroxylamine;neutral reaction; 液体发射药;硝酸羟胺;羟胺;中和反应;
Keywords liquid propellants;density specific impulse;monopropellant;bipropellant;atomic propellant; 液体推进剂;密度比冲;单组元推进剂;双组元推进剂;原子推进剂;
Acceptance testing equipment for production of liquid propellant. 生产液体推进剂用的验收试验设备。
Glyoxal is prepared with waste liquid propellant HNO3-27S and ethanal. 利用报废的液体推进剂硝酸-27S和乙醛制备乙二醛。
Some stratification exists in the spray produced by any liquid propellant injector. 由任何液体推进喷注器所产生的喷雾都存在某些成层现象。
The application of a pressure difference across an injector does not cause an immediate velocity response of the liquid propellant. 经过喷注器的压降发生变化时并不马上引起液体推进剂速度变化。
Liquid propellant combustion processes are quite complicated and defy precise analytical description. 液体推进剂燃烧过程是相当复杂的，很难对其进行严谨的分析描述。
Hydroxylammonium nitrate(HAN) is the main active toxic component of the new HAN based liquid propellant. 硝酸羟胺(HAN)是新型硝酸羟胺基液体推进剂的主要毒理活性成分。
Well and layer selection criteria of liquid propellant high energy gas fracturing (HEGF) are included in this paper. 提出了液体药高能气体压裂选井、选层的条件。
Oxidized starch,as a green corrosion inhibitor,was produced by abandoned liquid propellant of HNO_3-27S and starch. 本研究提出利用报废的液体推进剂硝酸-27S和淀粉反应制备氧化淀粉绿色阻垢剂,并对产品结构进行了表征。
To appreciate the unsteady environment existing in liquid propellant rocket chambers it is necessary that the steady state be well understood. 为了分析液体推进剂火箭发动机燃烧室中存在的非稳态环境，必须很好地了解稳态状态。
Two kinds of monolayer cobottom tanrs which store N2O4 and UDMH liquid propellant are used in many launch vehicles in foreingn countries. 国外较多的运载火箭上，采用二种类型的单层共底贮箱存放N2O4（四氧化二氮）、UDMH（偏二甲肼）液体推进剂等。
It is an important and basic issue to choose monitoring parameters of Liquid propellant Rocket Engine (LRE) monitoring system in ground test. 摘要确定监测参数是液体火箭发动机地面试验监控系统的一个重要而基础的问题。
The dynamic models of engine parts in a new high-performance staged combustion cycle liquid propellant rocket through the module codified were built. 通过模块化编程，建立了新一代高性能补燃发动机启动过程的部件模型。
Abstract： Objective To establish model of the blast-toxicosis combined injury caused by the explosion of the liquid propellant. 摘要：目的复制冲击波和液体火箭推进剂中毒致冲毒复合伤的动物模型。
Rapid reactions between liquid propellants can lead to inefficient mixing. 液体推进剂之间的迅速反应可能导致混合不良。