火箭的級 的英文怎麼說

中文拼音 [huǒjiànde]
火箭的級 英文
rocket stage
  • : fire
  • : 名詞(古代兵器) arrow
  • : 4次方是 The fourth power of 2 is direction
  • : Ⅰ名詞1 (等級) level; rank; grade 2 (年級) any of the yearly divisions of a school course; gra...
  • 火箭 : [航空] rocket; fire arrow; bird
  1. In this thesis, based on pershing ii surface to surface missile, a new kind of ballistic missile was designed with an additional rocket engine, which can be ignited twice. firstly, aerodynamic computational models of missile body and warhead which reentry with supersonic are built according to the task requirements ; secondly, the propulsion system model of missile is built whose first two stages are solid rocket engines and the third stage is liquid - solid combined rocket engine. the nozzle and the shape of the engine are designed to meet the needs of the populsion project ; thirdly, the trajectory model of the mass point is built and a wavy trajectory is designed & optimized ; finally, the ability of a missile ' s breaking through defence is analyzed

    以美國潘興導彈為原型,增加可兩次點發動機,改裝成具有跳躍能力地地彈道導彈;首先,根據任務需求,建立了導彈氣動模型,並建立了彈頭再入時高超聲速氣動模型;其次,建立了導彈推進系統模型,前兩採用了固體發動機,第三採用了固?液組合發動機,並在總體方案要求下,對發動機噴管和外形進行了設計;第三部分,建立了導彈質點彈道模型,設計了一條跳躍式彈道,並對跳躍式彈道進行了優化設計;最後,對導彈進行了突防能力分析,從分析結果可以看出,跳躍式彈道突防能力比常規拋物線彈道要強。
  2. Rocket based combined cycle ( rbcc ) will be one of the promising propulsion systems for single stage to orbit vehicle, and has extensively application foreground in both military and civil usage

    基組合循環發動機( rbcc : rocketbasedcombinedcycle )是單入軌最有潛力動力方案之一,具有廣泛軍事和民用航天應用前景,受到世界各國航天界矚目。
  3. Abstract : solid propellant rocket motors are preferred for most ballistic missiles because they need simple maintenance and can be launched quickly. but the conventional thrust termination devices limit the depletion of every stage ' s grain and increase some extra - weight. an improved method for designing a multi - stage solid rocket based depleted shutdown was provided. in order to solve the problem of lack of thrust termination devices, a device to adjust the burnout angle will match the final burnout velocity and satisfy the desired range. the method can also limit the detection from anti - ballistic missile system

    文摘:由於維護簡單和發射快速,彈道導彈多用固體發動機,但繁雜推力終止裝置使各裝藥不能耗盡並讓結構增重.提出了一種對基於耗盡關機多固體概念設計改進方法,此方法滿足導彈系統主要戰技要求.為解決無推力終止裝置末速不準問題,可在末發動機採用姿態調整裝置,對射角進行調整,配合末速以滿足射程要求.本方法還可抑制敵方反導探測
  4. 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發展歷程,介紹了9種最具代表性固體發動機技術特徵、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探空、運載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發展水平
  5. 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發展歷程,介紹了9種最具代表性固體發動機技術特徵、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探空、運載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發展水平
  6. One of the ways to make step rockets is to put the stages side by side at the bottom

    製造多一種方法是把各並排放在底部。
  7. The v-2 pushed the two-stage rocket to an altitude of 20 miles and then broke away.

    V2將第二推到20英里高度,然後脫落。
  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,為我國研究運載空中發射技術提供必要技術儲備。
  9. A top israeli general is warning that israel will turn the northeastern gaza strip into a demilitarized zone, if palestinian rocket fire into nearby israel continues

    一名以色列高將領警告說,如果巴勒斯坦人繼續向附近以色列城鎮發射,以色列將把加沙地帶東北部地區變為非軍事區。
  10. Both advantages of rocket engine and air - breathing engine are integrated into one kind of propulsion system, called rocket - based - combined - cycle ( rbcc ), which has multiple operating woke modes, including ejecting, subsonic combustion, supersonic combustion and rocket mode, with each mode operating at varying flying stage. rbcc has prominent potential of high efficiency and low cost, and so it is recognized as an advanced propulsion system of future single - stage - to - orbit reusable spacecraft and hipper - sonic missile. it has been broadly investigated in foreign countries and has been progressed into small and full - scale flying stage

    基組合動力循環( rbcc , rocketbasedcombinedcycle )將傳統發動機和吸氣式發動機優點集中組合到一個具有多種工作模態(包括引射、亞燃、超燃及模態)發動機里,在不同飛行階段啟用不同工作模態,因此具有大幅提高航天推進系統經濟性與高效性潛在優勢,並可能發展成為下一代單可重復使用航天器以及高超聲速導彈武器動力系統。
  11. 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,中國運載研究院,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計量檢測儀器。
  12. 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運載推進劑箱一個關鍵部件,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
  13. 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,驗證飛行器與運載分離時相關運動學和動力學問題。包括:飛行體質心運動和剛體運動;不同飛行體之間相對運動;不同飛行體上特殊部位之間相對運動;分離過程中各相關飛行體上載荷分析和分離過程中可能發生碰撞問題。
  14. The first - stage vehicle is used to launch the rocket and is then jettisoned in the upper atmosphere

    第一運載是用來發射,進入高層大氣后即拋掉
  15. After the first stage burns out, it falls back to earth along a parabolic path, while the engines of the second stage fire to thrust the rocket into an earth orbit

    當第一燒毀后,沿拋物線軌道落到地球,而第二發動機點發射到地球軌道。
  16. The trigger - happy steve francis and cuttino mobley were shipped to orlando in return for superstar guard / forward tracy mcgrady who now dons the rockets ' red

    亂槍打鳥史蒂夫?弗朗西斯和卡蒂諾?莫布里被送往奧蘭多,得到回報是超明星,鋒衛搖擺人特雷西?麥格雷迪,他現在穿著紅色。
  17. Four identical strap - on first stages allow heavy payloads to be deployed

    四支集束一有助提高運載能力。
  18. The regularlty of the maximum velocity ' s change for multi - stage rocket of parallel type when the effective jet velocity of every stage increases in order

    有效噴速依次遞增時並聯型多最大速度值變化規律
  19. The multi - stage rocket will jettison its aft stages when fuel in these stages is exhausted. this reduces the weight of the rocket and increases its speed

    會把燃料用完尾一依次分離丟掉,以減輕重量及增加速度。
  20. 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,體驗和學習回轉儀原理此外,觀眾可發射一枚多。播放影碟節目,則介紹運載成功發展。
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