missile body信息详情
导弹弹体
missile───adj.导弹的;可投掷的;用以发射导弹的;n.导弹;投射物
regulus missile───雷格斯导弹
fagot missile───法格特导弹
cruise missile───n.巡航导弹;n.[航][军]巡航导弹
missile defense───导弹防御
blowgun missile───喷枪导弹
deflect missile───偏转导弹
body body───身体
guided missile───导弹;导向飞弹;有线导引飞弹;n.导向飞弹,导弹
Then, a new design scheme of strap-down antenna stabilization system was proposed based on the analysis to 3D movement relationship of missile body, seeker, and antenna.───然后 基于弹体、导引头、天线的三维运动关系,提出了一种新型捷联天线稳定 系统控制方案。
The manufacture of phased array seeker is faced with some key techniques, such as complex electromagnetic environment, target stealth, disturbance of missile body, movement...───研制相控阵导引头面临复杂电磁环境、目标隐身、弹体扰动、弹目机动和专用微波组件等关键技术。
Finally, by using the ANSYS program, the thermal vibration characters of the plate and missile body structures with different materials is analyzed.───最后,采用ANSYS程序分析了合金材料、复合材料的板、弹体结构的热振动特性。
The visual-velocity increment and angle increment of missile body between samplings could be obtained by compensation algorithm.───通过补偿计算,能够得到弹体在采样时间间隔内运动的视速度增量和角增量。
The basic variant DF-11 features four large stabilising fins at the bottom of the missile body, but they are removed on the DF-11A.───基本型DF-11的特点在导弹的弹体底部有四个较大的稳定翼,但是它们在DF-11A上被移除。
Guided missile body before launched is influenced by the vibration of aircraft, creating elastic vibration.───说明了导弹发射前弹体受到载机振动的影响,产生弹性振动,振动对弹体结构、内部仪器造成损坏。
According to a new type of missile body structures, there is a study of the missile separation dynamic problems.───根据一种新型弹体结构,研究了导弹的分离动力学问题。
But this system can't get proportional guidance instruction directly because the antenna system is mounted on missile body.───但是采用该体制后,天线是固定安装在弹体上的,无法直接提取比例导引指令,必须寻求新的解决方案。
Air-admission mechanism and low speed tunnel test of a submerged inlet with low RCS missile body───一种隐身外形弹体下埋入式进气道的进气机理与低速实验研究
The major scattering resource in top direction is radar antenna or infrared head, in side direction is dihedral reflector formed by missile wings, missile body and wings.
Then, a new design scheme of strap-down antenna stabilization system was proposed based on the analysis to 3D movement relationship of missile body, seeker, and antenna.
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