rocket design 中文意思是什麼

rocket design 解釋
火箭設計
  • rocket : n 火箭；火箭彈，火箭發動機；火箭式投射器；〈英俚〉斥責。 a carrier [freight] rocket 載運火箭。 an...
  • design : vt 1 計劃，企圖，立意要…。2 指定，預定；留給，留著。3 設計，草擬，擬定，籌劃；起草，畫草圖，打（...
  1. Design method for aft - end igniter of small - scale solid rocket motor

    小型固體火箭發動機尾部點火器設計方法
  2. Design optimization for solid rocket motor based on graph morphing

    基於圖形變形法的固體火箭發動機優化設計
  3. Design of the multiple rocket launcher loading training simulator based on vr

    的火箭炮裝填訓練模擬器的設計
  4. Web - based integrated design platform for solid rocket motor

    的固體火箭發動機集成設計平臺
  5. Uncertainty optimization design of solid rocket motor grain

    固體火箭發動機裝藥不確定性優化設計
  6. Building on design work that began in 1996, scaled composites began developing a launch aircraft called the white knight, a three - seat rocket plane known as spaceshipone and associated ground operations [ see illustrations on pages 92 to 94 ]

    縮尺復合公司以1996年開始進行的設計為基礎，發展一架發射飛機白騎士、一架三人座火箭飛機太空船一號，和相關的地面操作系統（見88 ~ 90頁圖） 。
  7. For one thing, they simplify the design of a rocket engine.

    首先，它們可以簡化火箭發動機的設計。
  8. This paper relies on country 863 project " taking off levelly, two stage to orbit and transatmosphere flight vehicle system design ", research towed flight dynamics primarily, development for our country air launch technology of carrier rocket, offering the essential technological reserve

    本論文以國家863項目「水平起飛兩級入軌跨大氣層飛行器總體設計」為依託，對牽引飛行動力學進行初步研究，為我國研究運載火箭空中發射技術提供必要的技術儲備。
  9. Design optimization of chamber pressure and nozzle area expansion ratio of solid rocket motors

    固體火箭發動機燃燒室壓強及噴管擴張比優化設計
  10. It has been maked for immediate and statistical analysis that the calculation about the work order parameter of the base - bleed - rocket is calculated in the taguchi method, its influencing trend is bring out in the open, the theoretical base is settled for confirming the greatest combination about the work order parameter of the base - bleed - rocket. the multi - objectile optimal design model is established that the indexes have been taked into account first and synthetically, such as physical parameter range lethality power strength and flight stability and so on, the program is compiled and the example is calculated. the true worth of the theoretical work in this paper is validated by flight experimentation of 130mm hybrid base - bleed - rocket extended - range principium projectile

    本文進行了底排?火箭復合增程彈工作時序參數正交試驗設計的直觀分析與方差分析，揭示了每個參數對射程計算的影響趨勢，為進一步確定底排?火箭工作時序參數值的最佳匹配組合奠定了理論基礎；建立了底排?火箭復合增程彈多目標優化設計模型，該模型首次綜合考慮了底排?火箭復合增程彈的結構特徵參量、結構強度性能、飛行穩定性、威力性能和射程指標，編制了相應的分析程序，進行了算例計算；完成了130mm底排?火箭復合增程原理樣彈的結構設計與飛行試驗，其試驗結果驗證了本文理論研究工作的實際應用價值。
  11. Design of artillery rocket fault detection system

    火箭炮故障檢測系統設計與實現
  12. Electrostatic protection design of safe - launch rocket

    某型火箭彈安全發射靜電防護設計
  13. This paper discusses the design principles of rocket designing, engineering database and planar, three - dimensional accessory and constructional drawing in detail, including the dynamic assemble process. in the same time, the correlative result is given

    文中對火箭彈設計理論、工程數據庫的設計和二、三維零件圖、裝配圖的設計開發過程進行了詳細的闡述，給出了相應部分的設計結果。
  14. The design of the rocket nozzle also has much to do with the behavior of the exhaust and the resulting velocity of the vehicle itself.

    火箭噴管的設計與排氣的性能及飛行器本身的有效速度也有很大關系。
  15. In other cases, civil engineers are assigned to work on a project in another field ; in the space program, for instance, civil engineers were necessary in the design and construction of such structures as launching pads and rocket storage facilities

    另外土木工程師還會被安排到另一些領域區工作，如太空開發計劃，在設計和建造一些結構如火箭發射架和儲存設施時，土木工程師就有必要參與其中的設計和建設。
  16. After introduction of the whole fpga design of b3g downlink, chapter four schemed out every function module such as time synchronization, frequency synchronization, timing recovery, last frame detect, ofdm demodulation and rocket i / o interface etc. lots of structure schemes and simulation waves were presented

    主要包括時間同步模塊、頻率粗同步模塊、頻率精同步模塊、定時恢復模塊、尾幀檢測模塊、 agc / afc輔助模塊、 ofdm解調模塊和rocketi / o介面模塊等。
  17. Gap design of solid rocket motor nozzle was analysized through thermal and structure analysis

    摘要通過熱和結構計算，對固體火箭發動機噴管縫隙設計進行了分析。
  18. Using method of sumt and powell, the thesis carries out optimization design for air rocket with double - push accelerated velocity and spin - rate regularity, which dramatically decreases air rocket dispersion. in the end, some valuable conclusions are achieved for application

    綜合利用雙推力加速度，轉速規律，同時採用內點罰函數法和powell共軛方向法，對航空火箭彈的主要參數進行優化設計，實現了大幅度減小航空火箭彈散布的目的，得到了一些有應用價值的結論。
  19. Arde aircraft and rocket design engineers

    飛機與火箭設計工程師
  20. Rocketcad system has been proved to be an excellent prior and posterior cad system of rocket designing in practice. it can automate the rocket design process, provide the academic foundation to improve the structural design of rocket accessory, and also it can be used as a cai software for students of rocket weapon

    實際應用證明，使用rocketcad系統可以較好解決火箭彈前設計和后設計問題，實現了設計過程的自動化，為優化結構設計提供了理論依據，同時也可以做為火箭武器專業的計算機輔助教學（ cai ）軟體使用。
分享友人
分享到 Line

分享到臉書