運載火箭級 的英文怎麼說

中文拼音 [yùnzǎihuǒjiàn]
運載火箭級 英文
launch-vehicle stage
  • : 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 ...
  • : fire
  • : 名詞(古代兵器) arrow
  • : Ⅰ名詞1 (等級) level; rank; grade 2 (年級) any of the yearly divisions of a school course; gra...
  • 運載 : carry
  • 火箭 : [航空] rocket; fire arrow; bird
  1. The evolution course of chinese solid rocket propulsion technology for space missions since 1950s is presented. the technical features, development process, ground tests and flight records of nine typical solid motors are described. these motors were developed for sounding rockets, upper stages of launch vehicles and orbit transfer systems in application satellites respectively. the evolution of basic technology of chinese solid rocket motors and future developing concept are briefly introduced. the information in the paper are all based on the published literatures

    敘述了20世紀50年代以來中國航天固體推進技術的發展歷程,介紹了9種最具代表性的固體發動機的技術特徵、研製過程、地面試驗和飛行情況,這些發動機分別應用於中國的探空上面和應用衛星變軌系統.文中還簡要地評述了中國固體推進各單項技術的發展水平
  2. Abstract : the evolution course of chinese solid rocket propulsion technology for space missions since 1950s is presented. the technical features, development process, ground tests and flight records of nine typical solid motors are described. these motors were developed for sounding rockets, upper stages of launch vehicles and orbit transfer systems in application satellites respectively. the evolution of basic technology of chinese solid rocket motors and future developing concept are briefly introduced. the information in the paper are all based on the published literatures

    文摘:敘述了20世紀50年代以來中國航天固體推進技術的發展歷程,介紹了9種最具代表性的固體發動機的技術特徵、研製過程、地面試驗和飛行情況,這些發動機分別應用於中國的探空上面和應用衛星變軌系統.文中還簡要地評述了中國固體推進各單項技術的發展水平
  3. 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,為我國研究空中發射技術提供必要的技術儲備。
  4. Di - on electrics service and products cover the power electric field including power generation transmission distribution, power equipment manufacturing, subway, utilites, ac dc metrology field as well, more than 500 units of electric power utilities and stations such as beijing power supply bureau, guangzhou power supply bureau, baosteel, three gorges power station and more manufacturers like siemens, abb, alstom, bicc, pirelii, toshiba and more and 30 units of metrology institutes in china like nim, tsinghua university and more are our user. di - on electric is sole and exclusive distributor for numerous famous companies like transinor doble norway, measurements international canada, ndb canada, schuetz germany, aan germany, dr. strauss germany and etc, taking care of their business and service in p. r. china including hongkong

    絕大多數員工擁有本科和研究生以上學歷,在電力系統和計量系統工作多年,從事電力檢測帶電監測和計量測試儀器的技術服務和市場銷售工作長達10年以上,為約500多家電力工業系統的發供電部門如北京供電局,廣州電力局,深圳供電局,三峽電廠,廣州抽水蓄能電廠,田灣核電站等等,科研調試部門如廣東省電力試驗研究所,湖北省電力試驗研究所等等與設備生產廠如siemens , abb , alstom , toshiba等等提供了國際最先進可靠的測試技術和儀器設備為約30多家國內二以上相關計量科研院所,包括國家計量院,清華大學,中國研究院,空間技術研究院,航天二院,成飛,西飛和各省市計量院,電力試驗研究院所等提供了大量最先進可靠的計量檢測儀器。
  5. During its storage, transportation, maintenance and service, the solid rocket motor ( srm ) may encounter many incidents such as being dropped onto the ground while being hoisted up, crashing when vehicle turns over during transportation, being struck heavily in takeoff or landing accident while being carried by airplane, impacting with launch platform or buildings when there is abnormality during launch of multiple - stage rocket. impact of great intensity takes place in such accidents, which will lead to srm ignition or explosion

    固體發動機在貯存、輸、維護及使用過程中可能遇到各種意外機械撞擊激勵,例如:吊裝過程中跌落,輸過程中因交通事故發生翻覆碰撞,機固體導彈掛飛時因機發生起降事故導致高速沖撞,多發射初期因發射異常與發射架或地面建築物發生碰撞等,固體發動機將受到劇烈機械撞擊荷作用,導致其著燃燒甚至爆炸。
  6. The large - scale honeycomb structure, an important component of the last stage fuel tank of launch vehicles, is composed of the honeycomb sandwich and thin aluminum alloy sheets with ellipsoid shape

    大型蜂窩共底構件是液體推進劑箱的一個關鍵部件,它是由蜂窩夾芯復合材料和上、下薄鋁合金蒙皮粘接固化而成的。
  7. Contact analysis of stage separation surface of carrier rocket

    運載火箭級間分離面接觸分析
  8. In the condition of non - axisymmetrical stage separation in hypersonic flight, the problems of dynamics and kinematics of the validating vechicle and the launch vechicle are primarily analysised. it includes the movement of the center of mass and the rigid body of the vechicles, the relative movement of the different vechicles, the relative movement of the special parts of the different vechicles, the load analysis and the probable collision in the process of stage separation

    研究了在高超聲速狀態下非對稱間分離過程中,驗證飛行器與分離時的相關動學和動力學問題。包括:飛行體質心動和剛體動;不同飛行體之間的相對動;不同飛行體上特殊部位之間的相對動;分離過程中各相關飛行體上的荷分析和分離過程中可能發生的碰撞問題。
  9. Abrv advanced ballistic re - entry vehicle

    彈道重返大氣層
  10. The first - stage vehicle is used to launch the rocket and is then jettisoned in the upper atmosphere

    第一是用來發射的,進入高層大氣后即拋掉
  11. Its main components include four liquid fuel boosters, first rocket stage, second rocket stage, fairing and escape tower. it is the longest and heaviest among all chinese launch rockets

    由四個液體助推器芯一芯二整流罩和逃逸塔組成,是目前我國所有中起飛質量最大長度最長的。
  12. Four identical strap - on first stages allow heavy payloads to be deployed

    四支集束一有助提高能力。
  13. Using the ipga and setting the terminal speed increment of the upper stage and the manufacture cost of cpkm as objective functions, the rocket motor are processed dual - objective optimization design that has six design parameters

    採用ipga演算法,以該上面末速度增量最大及cpkm發動機的製造成本最低作為目標函數,對該發動機進行了雙目標優化設計。
  14. They can also " launch " a multi - stage rocket in slow motion and trace the successful development of launch vehicles and their payloads through videodisc programmes

    觀眾可坐在回轉椅上,體驗和學習回轉儀的原理此外,觀眾可發射一枚多。播放的影碟節目,則介紹的成功發展。
  15. The optimization design of dfc is expounded and the concept and method of multiobjective optimization are used to the upper stage solid rocket motor ( cpkm ) of a kind of launching vehicle

    闡述了面向成本的優化設計問題,並將多目標優化概念和方法應用於某上面固體發動機( cpkm )方案設計。
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