maneuverable missile中文是什么意思

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中文翻译
造句

机动导弹

missile n. 投射器；飞射器[箭、炮弹等]，射弹，飞弹；导弹。 ...
maneuverable 便于驾驶的; 操纵灵敏的; 操纵性能良好的; 操作灵活的, 有机动性的; 机动的; 可操纵的; 可调动的; 容易操作的; 有机动性的
highly maneuverable 高度机动的; 机动性高的
maneuverable aircraft 机动性能好的飞机
maneuverable head 机动弹头
maneuverable landing 机动飞机着陆
maneuverable launcher 机动发射装置
maneuverable policy 机动灵活的政策
maneuverable satellite 机动卫星
maneuverable ship 操纵性能良好的船舶
maneuverable spacecraft 可机动的航天器
non-maneuverable 非机动的
highly-maneuverable aircraft 机动性好的飞机
maneuverable ballistic reentry vehicle 机动弹道式再入飞行器
maneuverable re-entry 机动再入技术
maneuverable reentry vehicle 可操纵返航运载工; 可操纵重板大气层飞般
maneuverable reentry vehicle (marv) 可操纵返航运载工
maneuverable space capsule 可操纵航天舱
small warhead and maneuverable reentry 小型弹头与机动再入
missile n. 投射器；飞射器[箭、炮弹等]，射弹，飞弹；导弹。 an air-to-air (guided) missile 空对空飞弹，机载飞弹。 an atom-tipped missile 原子弹头飞弹。 a homing missile 自动寻的飞弹。 an intercontinental ballistic missile 洲际弹道导弹〔略 I.C.B.M.〕。 an infrared homing missile 红外线寻的导弹，红外线自动导引导弹。 a staged missile 多级导弹。 a development missile 试验导弹。 n. -man 导弹制造者[设计者]；火箭发射手，导弹操作手；导弹专家。 n. -ry 导弹技术；导弹〔总称〕。
maneuverable re-entry ferry system 可机动的再入大气层运输火箭系统
antiballistic-missile missile 反弹道导弹的导弹
antiballistic-missile-missile battallion 反弹道导弹导弹营
antiballistic-missile-missile battery 反弹道导弹导弹连
antitactical-ballistic-missile missile 反战术弹道导弹的导弹

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例句与用法

The empty weight to total weight ratio of subsonic maneuverable missile was given experimentally
利用经验的预测方法对亚声速飞航导弹的空重比进行预测。
The mission section , the constrain conditions , the weight composition of the maneuverable missile , and the model of used in turbofan engine maneuverable missile were presented
简述了飞航导弹任务剖面、约束条件的给定、导弹的重量组成以及涡扇发动机模型。
The cycle parameters of missile for turbofan engine were optimized for meeting the demand of maneuverable missile , and the developing trend of missile for turbofan engine was predicted
根据飞航导弹的要求对涡扇发动机进行了循环参数优化选择并预测了未来涡扇发动机的发展趋势。
The performance of next generation maneuverable missile was predicted by taking into account its important parameters such as lift to drag ratio , empty weight to total weight ratio and effective load
在考虑导弹空重、有效载荷和气动特性的情况下，预测了未来先进飞航导弹的性能。
By using the method of aircraft and turbofan engine integrated analysis , a model of maneuverable missile and turbofan engine integrated optimum design was developed and the computational examples and the analysis were presented
摘要利用飞机涡扇发动机一体化设计的思路，建立了飞航导弹涡扇发动机一体化设计的优化设计模型并给出了算例和分析。
By using the method of aircraft and turbofan engine integrated analysis , a model of maneuverable missile and turbofan engine integrated constrain analysis and mission analysis was developed and the computative examples and the analysis were given
摘要利用飞机涡扇发动机一体化设计的思路，建立了飞航导弹涡扇发动机一体化设计的约束分析和任务分析模型并给出了算例和分析。
The constrain - analyzed results and the mission - analyzed results of some maneuverable missiles indicate that the model of maneuverable missile and turbofan integrated constrain analysis and mission analysis is feasible and available
对飞航导弹的约束分析计算结果和任务分析计算结果表明，建立的飞航导弹涡扇发动机一体化约束分析与任务分析模型是合理可行的，具有很好的工程实用价值。

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Last modified time:Mon, 11 Aug 2025 00:29:56 GMT