- 更多网络例句与火箭推进剂相关的网络例句 [注：此内容来源于网络，仅供参考]
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Since the danger was recognised action has been taken in the United States and in the European Economic Community to effect a decrease in the use of chlorofluorohydrocarbon as aerosol propellants.
to effect在句中做目的状语，主句为被动形式"美国以及欧洲共同体已经采取了行动，以减少作为火箭推进剂的氟氯烃的使用。"
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This paper develops a theoretical model of the heat radiation effect and the shock wave characteristics for liquid hypergolic rocket bipropellant explosion,as well as the explosion experimental method.
建立了自燃液体火箭推进剂爆炸热辐射效应和冲击波特性理论模型，介绍了实验研究的方法，给出了N2O4／UDMH液体推进剂爆炸产生的火球直径、火球温度、火球辐射热流、爆炸冲击波超压值等参数计算与实验观测结果，结果表明计算结果与实验观测结果吻合。
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Based on the three dimensional viscoelastic integral constitutive relation of a propellant grain with the finite element method, the analysis about the thermo-viscoelasticity of solid propulsive agent column is presented.
基于药柱的三维线性热粘弹性积分本构关系，采用有限元法，对固体火箭推进剂药柱进行热粘弹性有限元分析，得出药柱在轴向过载作用下的变形结果和药柱内危险部位的位置，表明药柱具有明显的粘弹性特点。
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This is an important consideration for its use as a rocket propellant.
这是一个重要的考虑因素，供其使用，作为火箭推进剂。
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These features of 〓 cluster will bring outthe innovative change for development and application of the rocket propellant.
的这些特性，将对火箭推进剂的研制和应用带来革新性的变化。
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This highly useful thermochemical software allows the user to evaluate the theoretical performance of a solid rocket propellant.
这非常有用热软件使用户评价理论的表现了坚实的火箭推进剂。
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The results showed that the performance of unchoked ducted rocket is superior to that of choked one. When the gas generator is loaded with high burning-rate exponent fuel-rich propellant, the performance of unchoked ducted rocket is almost the same as that of the ducted rocket working under fixed mass ratio of fuel to air.
研究结果表明：非壅塞固体火箭冲压发动机的性能显著优于燃气流量不可调的壅塞式固体火箭冲压发动机；当贫氧推进剂具有高的燃速压强指数时，非壅塞固体火箭冲压发动机的性能接近燃气流量完全调节、以等空燃比工作的冲压发动机性能。
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The burning surface of a rocket propellant grain recedes in a direction perpendicular to this burning surface.
燃烧表面的火箭推进剂药柱消退在一个方向垂直于这燃烧的表面。
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2 The measurement of temperature of solid propellant plume by remote sensing FTIR The infrared radiance spectra was obtained by remote sensing FTIR. The temperatures of four plumes of propellants and a infrared reagent were calculated according to the gas vibration rotation band fine structure such as CO, HF, H2O and HC1 in plume of solid rocket propellant. The results have a agreement with the theoretical data.
2.2 FTIR遥测固体推进剂羽流温度本文利用遥感FTIR测试技术测得了固体火箭推进剂羽流的红外辐射亮度分布图，并根据谱图中CO、HF、HZO、HCI四种气体振转谱带精细结构计算了推进剂羽流温度及红外辐射药剂的燃烧温度，计算结果与理论预测值基本一致。
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Hydroxylammonium nitrate-based liquid propellants have been pursued as liquid gun and rocket propellants for many years in America.
硝酸羟胺基液体推进剂作为火炮发射药和火箭推进剂，在美国已经使用多年，我国可能在不远的将来投入使用。
- 更多网络解释与火箭推进剂相关的网络解释 [注：此内容来源于网络，仅供参考]
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liquid, propellant：液体推进剂
liquid phase 液相 | liquid propellant 液体推进剂 | liquid propellant rocket 液体推进剂火箭
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liquid propellant rocket：液体推进剂火箭
liquid propellant 液体推进剂 | liquid propellant rocket 液体推进剂火箭 | liquid propellant rocket engine 液体火箭发动机
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liquid propellant sustainer：液体推进剂主发动机
liquid propellant starter | 液体推进剂启动机 | liquid propellant sustainer | 液体推进剂主发动机 | liquid propellant unit | 液体火箭发动机
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liquid propellant rocket engine：液体火箭发动机
liquid propellant rocket 液体推进剂火箭 | liquid propellant rocket engine 液体火箭发动机 | liquid seal 液封
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liquid propellant rocket engine：液体推进剂火箭发动机
liquid propellant rocket | 液体推进剂火箭 | liquid propellant rocket engine | 液体推进剂火箭发动机 | liquid propellant starter | 液体推进剂启动机
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multistage rocket：多节火箭
多节火箭(multistage rocket)是一种使用了两节或更多节的火箭,每节火箭皆搭载了自有的引擎及推进剂. 堆栈分节(stacked stage)的方式将一节装载在数节之上;平行分节(parallel stage)的方式则将一节装载在其它节的旁边. 使得二或更多个火箭互相堆栈或放置于其它火箭的旁...
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composite propellant：组合火箭推进剂
composite product | 复合材料制品 | composite propellant | 组合火箭推进剂 | composite reaction | (石油)组合反应
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liquid propellent rocket：液体推进剂火箭
液体推进剂 liquid propellant | 液体推进剂火箭 liquid propellent rocket | 受液器 liquid receiver
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solid rocket：固体火箭,固体燃料火箭
solid rock 坚岩 | solid rocket 固体火箭,固体燃料火箭 | solid rocket fuel 固体推进剂
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tripropellant rocket-power plant：三元推进剂火箭动力装置
triprolidine hydrochloride ==> 盐酸丙吡咯啶 | tripropellant rocket-power plant ==> 三元推进剂火箭动力装置 | tripropoxy butane ==> 三丙氧基丁烷