助推段彈道 的英文怎麼說

中文拼音 [zhùtuīduàndàndào]
助推段彈道 英文
boost trajectory
  • : 動詞(幫助; 協助) help; assist; aid; support
  • : 動詞1 (向外用力使物體移動) push; shove 2 (磨或碾) turn a mill or grindstone; grind 3 (剪或削...
  • : Ⅰ量詞(部分) section; segment; part; paragraph; passage Ⅱ名詞(姓氏) a surname
  • : 彈名詞1. (彈子; 小球形的東西) ball; pellet 2. (內裝爆炸物, 具有破壞和殺傷能力的東西) bullet; bomb
  • : Ⅰ名詞(道路) road; way; route; path 2 (水流通過的途徑) channel; course 3 (方向; 方法; 道理) ...
  1. The approximate solutions of the mid - course trajectories for the boost - glide vehicles are investigated

    摘要研究了滑翔式的近似解。
  2. Further more, the solutions of this paper is benefit for the estimation of the characteristics of this new trajectory, such as maximum heating rate, load factor and dynamic pressure during the period of the project demonstration

    研究結果可為新型滑翔式飛行器在方案論證階時的特性分析以及射程、峰值熱流和過載等特徵參數的估算提供依據。
  3. And the effect of the work order of the two propellant units to the performance of the trajectory and the matching conditions to obtain the theoretical optimum trajectory is discussed too. according to the ballistic speciality of a hybrid base - bleed - rocket extended - range projectile during base - bleed and rocket work, its physical parameter is non - constant, such as its mass position of mass centre polar and equatorial moment of inertia. after a mulriple ballistic model of constant physical parameter is established, a mulriple ballistic model of continuous and non - continuous physical parameter is educed and the program is compiled, the theoretical tool is constructed to study othe other pivotal technology of a hybrid base - bleed - rocket extended - range projectile

    本文根據底排?火箭復合增程其底排燃減阻和火箭的質量、質心位置、轉動慣量等結構特徵參量變化的特徵,在建立底排?火箭復合增程結構特徵參量為不變常量的多元計算模型基礎上,導出了結構特徵參量為連續變化量和非連續變化量的底排?火箭復合增程多元計算模型,編制了相應的計算機數值分析程序,構建了研究底排?火箭復合增程其它關鍵技術的理論工具。
  4. The processing method of rocket - assisted test data for rocket - assisted and base - bleed projectile

    復合增程火箭助推段彈道數據處理方法
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