運載器 的英文怎麼說

中文拼音 [yùnzǎiqì]
運載器 英文
capsule
  • 運 : Ⅰ動詞1 （物體位置不斷變化） move; revolve 2 （搬運; 運輸） carry; transport 3 （運用） use; wield...
  • 載 : 載Ⅰ名詞（年） year : 一年半載 six to twelve months; six months to a year; 三年五載 three to five ...
  • 器 : 名詞1. （器具） implement; utensil; ware 2. （器官） organ 3. （度量; 才能） capacity; talent 4. （姓氏） a surname
  • 運載 : carry
  1. In order to investigate the variety of some of the initiatory kinematics parameters, the author first computes the underwater trajectory of the submarine launched missile carrier

    為了摸清分離體在分離時刻的初始運動學參數可能的變化范圍，首先計算了導彈運載器的水下彈道。
  2. Vehicles ; apparatus for locomotion by land, air or water

    車輛陸上空中水上或水裡用運載器。
  3. In this article the calculative formula for ejecting mixer of vapor - water has been obtained, and the ejecting mixer has been designed in the under - water carrier ' s working environment

    本文推導了水蒸氣-水的噴射混合器的計算公式，設計了一臺針對水下運載器工作環境的噴射混合器。
  4. At last ejecting mixer by design has been validated through experiment, and it is showed that the tired heat produced by under - water carrier can be completely converted and released, and the design goal has been achieved

    本文最後通過實驗對所設計的噴射混合器進行了實際的驗證，實驗結果表明，利用噴射混合器完全能夠將水下運載器在工作過程中產生的乏熱轉換釋放，達到了設計要求。
  5. The paper has founded the model of laser transmission in launch process and the movement model of laser - powered vehicle, and has analyzed the influence on performance of launch system, which was raised by some factors, for instance, the performance of thruster, the attenuation in transmission, the height of mode - transform, the laser power, the air drag force, the launch height, and so on

    本文研究了激光推進微小衛星發射系統的概念和性能。建立了發射過程激光傳輸和激光推進運載器運動模型，分析了推進系統性能、大氣傳輸衰減、模式轉換高度、激光器功率、大氣飛行阻力、發射點高度等因素對發射系統性能的影響。
  6. Through calculating and analyzing basic performance, the flight characteristic of the towed system is researched. stability and control issue of carrier rocket is discussed primarily. the net result of the thesis will prove the feasibility of the scheme of towed launch

    論文通過牽引系統基本性能的計算和分析，完成牽引飛行特性的研究，同時對運載器的穩定性和控制問題進行初步的探討，最終結果將驗證牽引發射方案的可行性。
  7. According to purpose of the towed flight, a new trajectory consisting of taking off, climbing phase, level flight phase is presented with. trajectory pitch angle of the towing plane is optimized. according to the flight law of the towing plane, the fin deflection angle and amplification coefficient of particle - system trajectory of carrier rocket are designed, in order to realizing flight steadily of the carrier rocker

    根據牽引飛行的目的，對載機應用了「起飛?爬升?平飛」的變軌道飛行方案，同時對載機軌道的傾角、傾角變化規律進行優選設計；再根據載機的飛行規律，對運載器質點系軌道的舵偏規律及其放大系數進行了設計計算，實現運載器穩定牽引飛行。
  8. Ascend motion analysis of reusable launch vehicle

    可重復使用運載器上升段運動分析
  9. Abstract : with simulated annealing approach based on simple method, the dynamic system of some submarine - launched missile carrier s water trajectory is identified, and the effects of no - modeling uncertainty and dimension of parameters to be identified on overall identification precision are investigated

    文摘:運用基於單純形的模擬退火演算法對某潛射導彈運載器水彈道動力學系統進行了辨識，並探索了未建模不確定性及待辨識參數矢量的維數對辨識精度的影響。
  10. Secondly, towed system is considered as many rigid body systems. according to research approaches of many rigid body systematic dynamics, the towed systematic engagement calculating models is derived ; according to actual course of the towed flight, deriving mathematics model of the course of taking off and towed flight of the towing plane and of carrier rocket, and corresponding parameter calculate models

    其次將牽引系統作為多剛體系統宋考慮，根據多剛體系統動力學研究方法，建立牽引系統約束方程，由此推導出約束力計算公式；根據牽引飛行實際過程，推導出載機、運載器在起飛階段，巡航飛行階段的數學模型，以及相應的參數計算模型。
  11. Technical progress of reusable launch vehicle part

    國外可重復使用運載器的技術進展
  12. A study of the two - stage - to - orbit reusable launch vehicle scheme

    兩級入軌重復使用運載器的方案探討
  13. Class12 ： vehicles ; apparatus for locomotion by land, air or water

    類別12 ：車輛；陸上、空中、水上或水裡用運載器。
  14. Class 12 vehicles ; apparatus for locomotion by land, air or water

    商標注冊類別12車輛；陸上、空中、水上或水裡用運載器。
  15. Design of variable - structure attitude control system for rlv reusable launch vehicle

    可重復使用運載器變結構姿態控制演算法設計
  16. Finally, the system project of hx - based thruster vehicle was researched

    本文最後對熱交換器模式發動機運載器系統方案進行了研究。
  17. The predictor - corrector reentry guidance algorithm for reusable launch vehicles was studied

    摘要研究了可重復使用運載器的預測校正再入制導方案。
  18. The selection of the stage number for the reusable launching vehicle program based on life - cycle - cost analysis

    基於全壽命周期費用分析的可重復使用運載器級數選擇
  19. Then in this paper the author establishes the simulation model of the probability of smashing the submarine when the segregator of the submarine launched missile carrier sinking in the water and uses the monte carlo ( of or relating to a problem - solving technique that uses random samples and other statistical methods for finding solutions to mathematical or physical problems. ) to simulate the whole process. then the author carrier through much simulating computations and gives the smashing probability at different conditions

    在對分離體下沉的各種干擾因素進行了深入的分析后，建立了基於蒙特卡羅方法的潛射導彈運載器分離體砸艇概率的計算模型，並且進行了大量的計算機模擬試驗，分別對運載器採用平面彈道，偏航彈道在不同發射深度，不同發射艇速的情況下的分離體砸艇概率進行了模擬計算，給出了不同情況的砸艇概率。
  20. Later the author computes the underwater trajectory of the segregator of the submarine launched missile carrier, then discusses the influence to the underwater trajectory from the hydrodynamics parameters, collectivity parameters and the initiatory kinematics parameters

    而後根據初始運動學參數，計算了運載器分離體的下沉彈道，並且分別討論了分離體的總體參數、流體動力學參數和初始運動學參數對下沉彈道的影響。
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