research rocket 中文意思是什麼

research rocket 解釋
研究火箭
  • research : n. 1. 仔細搜索 （for, after）。2. 〈常 pl. 〉研究，調查，探測；追究。vt. ,vi. 追究；調查，研究 （sth. , into sth. ）。
  • 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. All the rockets ever assembledthe fireworks skyrocket, the ballistic missile, the big research rocket, the newest space rockethave one thing in common.

    過去製成的所有火箭，不論是花炮，彈道導彈，巨大的科研火箭，還是最新的宇宙火箭，它們都有一個共同點。
  2. At the same forum, their papers revealed new rocket propulsion research, including work on hybrid systems that use a combination of propellants easier to handle and store than most propellants in wider use today

    在本次論壇上，中國人的論文揭示了其新的火箭推進研究，其中包括一個混合系統，該系統使用了比今天廣泛應用的推進劑更容易貯藏和操作的多種推進劑組合。
  3. Space research activities are being aided through two sounding rocket lauching stations sponsored by the united nations.

    對于空間研究活動的援助是通過聯合國支助的兩個探空火箭發射站進行的。
  4. 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。
  5. In this paper, taking the rocket - assisted cartridge as the research object, systematic analyses and studies have been conducted on its ballistics characteristics. the whole ballistics is divided into three stages. different ballistics models and tested data processing methods have been determined according to the different characteristics on each stage

    本文以火箭增程彈為研究對象，在對其彈道特點進行系統的分析研究的基礎上，將全彈道分為三段，根據各段不同的特點導出了不同的彈道模型及測試數據處理方法。
  6. Because the propellant grain is viscoelastic material, the liner and adiabatic layer are also viscoelastic one, the interface debond problem is actually interface crack about elastic - viscoelastic or bi - viscoelastic materials. research about this problem relates to the knowledge of viscoelastic mechanics and interface fracture and combustion. numerical analysis method about interface debond on solid rocket motor is researched in this paper

    由於固體火箭發動機的推進劑藥柱是一種粘彈性材料，襯層和絕熱層也具有粘彈性性質，因此其界面脫粘問題實際上是彈性-粘彈性或雙粘彈性各向同性材料界面裂紋問題，對該問題的研究涉及到粘彈性力學、界面斷裂力學和燃燒學等相關學科。
  7. Through malfunction of the tests of 810 research institute, the combustion performance of the hybrid motor and model about regression rate have been studied in the dissertation. the main aspects are as follows : the performance of the hno3 + n2o4 - htpb hybrid rocket motor were all discussed

    本文結合航天科技集團公司810研究所正在研製的ak - 20l / htpb + al組合固液火箭發動機，開展了固液火箭發動機混合燃燒特性的數值模擬工作，在此基礎上給出固體燃料退移速率預示模型及預示結果。
  8. Research of initial disturbance of rocket in lagrange

    拉格朗日方法建模下的火箭彈起始擾動研究
  9. Rocket research has confirmed a strange fact which had already been suspected : there is a “ high - temperature belt ” in the atmosphere, with it center roughly thirty miles above the ground

    火箭研究證實了早就懷疑的這樣一個奇異的事實:大氣層中有一個「高溫帶」 ，其中心在距地面約30英里高的地方。
  10. Rocket research has confirmed a strange fact which had already been suspected there is a “ high temperature belt ” in the atmosphere, with its center roughly thirty miles above the ground

    人們早就懷疑，大氣層中有一個「高溫帶」 ，其中心在距地面約30英里的高空。利用火箭進行研究后，這一奇異的事實已得到證實。
  11. Research on grouting repair technique for grain cracks of solid rocket motor

    固體火箭發動機藥柱裂紋灌漿修補技術研究
  12. 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。
  13. The structure design and the performance research of supersonic inlet / combustor are key techniques for solid rocket ramjet

    超聲速進氣道及補燃室的設計與性能研究是固體火箭沖壓發動機的兩大關鍵技術。
  14. The pressurized 85 % h2o2 - pe hybrid rocket motor test system has been designed and built up for the research work. the hot firing tests and the shutdown - restart of the motor were successfully performed. 2

    設計和建造了85 h _ 2o _ 2 ? pe固液火箭試驗發動機和擠壓式固液火箭發動機試驗系統，並成功地進行了點火和再啟動。
  15. For the research requirement of the high g - load mobile missile srm, the work process of solid rocket motor under lateral overload is investigated by the use of theoretical analysis and numerical simulation methods involving the calculation of internal ballistics, the simulation of flow field and the analysis of structural integrity

    本文以高速機動防空導彈固體發動機研製需求為背景，採用理論分析和數值模擬方法，從內彈道計算、內流場模擬、結構完整性分析等幾個方面對橫向過載作用下固體火箭發動機工作過程進行了研究。
  16. Research rocket tank - this upgrade changes steam tanks into war engines, giving them a rocket - like attack versus air units. currently not active

    研究火箭坦克-這個升級項目可以把攻城坦克變為"戰爭機器" ，給它們火箭用以攻擊空中單位
  17. In addition, the usaf continues to fund development work of the aerojet ( formerly atlantic research ) variable flow ducted rocket ramjet system as a future propulsion option for an extended range aam

    此外，美國空軍繼續投資于航空噴氣研究所（原來的大西洋研究所）的可變噴流管火箭發動機系統，將其作為增程空空導彈的未來推進選項。
  18. This paper is one part of the uestc ’ s assignment ? ? “ the design and research of mimu ” 。 by the research for mems and the mems acceleration sensor, this assignment will finish a series of mimu system, which will be applied to the rocket and the missile guided system. this thesis mainly include following facets : research the mature mems processing technic at the present, develop a type of capacitive acceleration sensor which structure is simple and based on a set of new silicon bulk micromachining process

    本論文來自電子科技大學機械電子工程學院的課題「 mems慣性組合的設計與研究」 。該課題希望通過對mems技術和mems慣性傳感器的研究，研製和設計出一系列能夠應用於火箭和導彈制導的mimu系統。主要進行了一下工作:研究了目前較為成熟的mems加工工藝，提出了一種結構簡單，基於各向異性體硅微加工技術的電容式加速度傳感器。
  19. 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
  20. 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。
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