carrier rocket 中文意思是什麼

carrier rocket 解釋
運載火箭
  • carrier : n 1 運送人，搬夫；負荷者；使役，〈美國〉信差，郵遞員；送報人；〈英國〉運輸行，運輸業者。2 傳書鴿...
  • 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...
  1. 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。
  2. 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。
  3. 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。
  4. The astronaut yang liwei, spirited and assured, made his way into shenzhou - 5, the largest manned spacecraft in the world up to this time. on his shoulders rested the task of achieving glory for the nation. armed with courage and propelled by a sense of responsibility, he was ready for the momentous journey into space. shenzhou - 5 was launched into space by the changzheng - 2f carrier rocket, nicknamed the " magic arrow "

    二零零三年十月十五日早晨，酒泉衛星發射中心一切就緒，航天員楊利偉英姿勃發，神情自若，步入目前世上可用空間最大的載人飛船神舟五號，肩負為國爭光的大任，心懷雷霆不移的大勇，責無旁貸，義無反顧，踏上了乘雲陵霄、遨遊穹蒼的征途。
  5. Contact analysis of stage separation surface of carrier rocket

    運載火箭級間分離面接觸分析
  6. 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。
  7. As far as the system observation for accuracy evaluation of carrier rocket is concerned, there may exist different types of observed data and priors. heterogeneous information means that the different information describing the different characteristics of the same object. since all of the information is relevant to the same object, the fusion is possible. it is a key problem that how to fuse the heterogeneous information to obtain the better evaluation result. therefore, the different heterogeneous information and data is thoroughly studied, moreover, the mathematical description for information fusion of different parameter priors and data is constructed in this paper. based on their relationship between different parameters, indirect prior and observation data is transformed into prior in impact point observation space, which is fused with original prior by weight determined by maximum entropy rule to obtain the mixed posterior distribution. therefore, the test results can be given by combining posterior distribution and impact error observed data. then its application on evaluating guidance systematic error is elaborated as it applies trajectory tracking data, test value of coefficients of guidance instrumentation systematic error, impact point observation data and prior. especially, the advantage of this method lies in its application in case that guidance instrumentation systematic error may not be computed precisely. finally a detailed example on evaluation of carrier rocket is given to verify the theory

    為充分利用運載火箭觀測中的不同觀測空間和過程的信息來進行精度評估，針對該背景建立了異質先驗融合的數學描述.研究了飛行試驗中不同觀測空間和過程的異質先驗信息和數據，基於不同觀測過程的解析關系，將間接過程的先驗和觀測數據算出的后驗分佈轉換成落點觀測空間上的先驗，與原落點的先驗進行了最大熵加權融合，得到混合后驗分佈，從而結合落點觀測數據給出評定結果.在無法解算出精確的制導工具誤差系數的情況下，這種方法充分利用了彈道跟蹤數據、工具誤差系數的地面測試先驗值、落點先驗及落點數據，穩健性更好，準確性更高
  8. New generation carrier rocket system is a complicated system which requires high reliability. in principle, any fault is not allowed when the rocket is launching

    新一代運載火箭系統是一個極其復雜的系統，可靠性要求極高，原則上不允許運載火箭系統在發射過程中出現任何故障。
  9. China has started to make carrier rocket responsible for lauching the no. 7 shenzhou spaceship, which expected to launch in 2008

    中國已開始製造承擔神舟七號飛船發射任務的運載火箭，預計將在2008年發射。
  10. China has already begun to make a carrier rocket that will undertake the task of lauching the shenzhou number seven airship, which will be lauched in 2008

    中國已開始製造承擔神舟七號飛船發射任務的運載火箭，預計將在2008年發射。
  11. It will be launched by a russian carrier rocket and it is expected to land on mars with a russian probe in 2010 after 10 month ' s flight

    它將由俄羅斯運輸火箭發射並預計將歷經10個月的飛行於2010年和俄羅斯探測儀一同登錄火星。
  12. The gas supply system in the launch area offers compressed air 、 high - purity nitrogen and high - purity helium for carrier rocket 、 spacecraft test 、 fueling and satellite launch, which is an important part of the ground service support system in the launch area

    發射場配氣系統為運載火箭和衛星測試、加註、發射提供壓縮空氣、高純氮氣和高純氦氣，是發射場地面勤務系統的重要組成部分。
  13. On carrier rocket engine working - process research system model and its application

    運載火箭發動機工作過程研究體系模型的研究
  14. A preliminary discussion on automatic assembling and disassembling technotogy in liquid propellant robots of carrier rocket

    運載火箭液體推進劑機器人自動加泄技術初探
  15. Civil aerospace technologies have made remarkable achievements in the applied satellite, carrier rocket, and manned spaceship

    民用航天在應用衛星、運載火箭技術、載人航天等方面取得長足進步。
  16. People with even slight scientific knowledge will know that a carrier rocket is developed on the basis of ballistic missiles

    稍有科技常識的人都知道，運載火箭是在彈道導彈的基礎上發展起來的。
  17. Although oux carrier rocket engine technology has obtained tremendous advancement, it has much gap from the advanced country

    我國的運載火箭發動機技術雖然取得了巨大進步，但與世界先進水平相比仍有一定的差距。
  18. The key factor which effects carrier rocket engine technology is the deficiency of the ability of research and irmovation in carrier rocket engine

    影響我國火箭發動機技術進步的關鍵因素在於發動機研究、創新能力不足。
  19. The paper anaiyzes the key elements which affect the ability of rescarch and innovation of different kinds of engines. the author raises the conception of carrier rocket engine working process research system : builds the structure model of carrier rocket engine working process research system by using the theory of operationai research and systems engineering : analyzes this structure model by the analytical hierarchy process : calculates the system element important degree and integrate important degree. the research result has some reference values to the rocket engine research institute building and strategy development

    論文分析了影響不同類型火箭發動機研究、創新能力的各種因素，提出了運載火箭發動機工作過程研究體系的概念；綜合應用系統工程、運籌學理論，建立了運載火箭發動機工作過程研究體系結構模型；對工作過程研究體系結構模型進行了層次分析，確定了體系的層次結構；分析了體系中各個要素的相對重要程度及綜合重要程度。
  20. Abstract : digital simulation scheme for the pitch program control system of the carrier rocket is presented in this paper based on xxx and emphasized on the scheme " s realizing method, functional block and technological character

    文摘:以某型火箭為例介紹了運載火箭俯仰程序控制系統全數字模擬的實現方案，重點分析了其實現途徑、功能模塊和技術特點。
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