火箭艦 的英文怎麼說

中文拼音 [huǒjiànjiàn]
火箭艦 英文
rocket shi{lsmr
  • : fire
  • : 名詞(古代兵器) arrow
  • : 名詞(大型軍用船隻; 軍艦) warship; naval vessel; man-of-war
  • 火箭 : [航空] rocket; fire arrow; bird
  1. Returning to a theme he has voiced many times before, the cambridge university cosmologist said that space - rockets propelled by the kind of matter / antimatter annihilation technology popularised in star trek would be needed to help homo sapiens colonise hospitable planets orbiting alien stars

    這位劍橋大學宇宙論者重提他過去曾多次探討的主題說,星奇航記中那種廣為人知的物質?反物質的互相抵消科技推動的太空,可以用來幫助人類移民到環繞外星球運行的友善行星。
  2. Everytime you launch a support - rocket, the holdingtime is extended by the time interval in which the fleet uses the deut

    而每次你發射一枚補給,駐扎時間就會依據駐扎隊的用油量得到延長。
  3. Well, the iranian military has all kinds of rockets and missiles set to hit at least one of the carriers and other ships there in a short space of time, and they all will just disappear in a flash of smoke as a sacrifice by bush to promote the war

    與此同時,伊朗軍隊已經準備好了所有的和導彈來迅速擊沉至少一艘航空母和其他軍,這個隊將在烈中灰飛煙滅,成為了布希嗜戰的殉葬品。
  4. Effectiveness evaluation of the plan for multiple launcher rocket system on a warship

    載多管炮武器系統方案總體效能評估
  5. The servo motion dynamics of the ship - borne rocket launcher under the condition of ship sway is studied

    摘要該文研究了某炮在船搖擺情況下隨動系統調炮時的炮受力問題。
  6. The results provide calculational basis to the aiming mechanism design of ship - borne rocket launcher system

    計算結果為炮瞄準機的設計提供了依據。
  7. The model of ship - borne rocket launcher system is simplified and built by virtual prototype technology

    通過虛擬樣機技術對炮系統進行簡化和建模。
  8. Collaborative optimization method is studied in depth, the causes leading to computational difficulty of this method are discussed by optimization theory and computation examples, and improve method which may solve this problem is presented. based on the comparison of several optimization methods and the characteristics of modern rocket - ramjet, step optimization pattern - a new integrated design mode is presented and is used to realize integrated design of rocket - ramjet. inner and outer fiowfield of a certain integral rocket - ramjet missile is simulated numerically using n - s equation

    ( 2 )系統地研究了導彈總體優化設計方法,探討了多學科設計優化的原理、框架結構、具體表述形式,深入研究了協作優化方法的原理,從優化原理和算例兩方面討論了造成協作優化方法計算困難的原因,提出了可能克服這種計算困難的改進途徑;在比較幾種優化方法的基礎上,針對新一代沖壓式導彈的特點,提出了一體化設計的模式? ?分步優化模式,進行了整體式沖壓發動機反導彈總體參數的一體化設計。
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