推力器 的英文怎麼說

中文拼音 [tuī]
推力器 英文
thrust meter
  • : 動詞1 (向外用力使物體移動) push; shove 2 (磨或碾) turn a mill or grindstone; grind 3 (剪或削...
  • : Ⅰ名1 (力量; 能力) power; strength; ability; capacity 2 [物理學] (改變物體運動狀態的作用) forc...
  • : 名詞1. (器具) implement; utensil; ware 2. (器官) organ 3. (度量; 才能) capacity; talent 4. (姓氏) a surname
  • 推力 : visatergo; soot; propulsive force; thrust; momentum thrust
  1. The laser micro - thruster and its key technologies

    激光微推力器及其關鍵技術
  2. The investigation shows that plenum chamber total pressure has multifarious effects on arcjet thruster operation, and both specific impulse and thrust efficiency can be improved by increasing it befittingly under steady arc

    研究表明,集氣腔總壓對推力器工作過程具有多方面的影響,在保證電弧穩定的情況下,適當提高集氣腔總壓可同時提高比沖和進效率。
  3. A three layers thruster was designed. the middle layer was chamber, the top layer was ignition circuit and the bottom layer contained a diaphragm with several nozzles. it could integrate 4 micro - thruster which diameter was 0. 8mm on the diaphragm with 10 * 10 * 2mm

    在實驗中,設計了三層的推力器結構,中間為藥室,上層和下層為點火電路和帶噴管的蓋片,可以在10 10mm和2mm厚的板上集成了4個直徑為0 . 8mm的微推力器
  4. A test device was designed which tested the properties of thrust according the theory of electromagnetism scale. using the hall - effect sensor to measure the scale displacement that could be converted the magnitude of the thrust

    根據電磁天平的原理設計了一套微測試裝置,利用霍耳傳感來測量產生的位移,進而通過計算轉換為推力器大小。
  5. With advantages of simple and reliable in structure, high isp and easy control over a wide range of thrust, pulsed plasma thruster ( ppt ) is very suitable for micro - satellite ' s orbit control and high precision attitude control

    脈沖等離子體推力器( ppt )具有結構簡單可靠,比沖高,在較大范圍可控的特點,適合用於微、小衛星軌道控制和小衛星高精度姿態控制,其研究和應用得到了重視。
  6. For example, if one of the actuator fails, conventional feedback algorithms can no longer position a spacecraft to arbitrary orientation while this algorithm remains viable. preliminary investigations of the mpc approach to attitude control lead to the following conclusions : i

    例如:如果飛行三軸推力器中的某一軸發生故障,那麼常規的反饋演算法將無法把飛行定位到給定的方向,但f - mpc演算法則可勝任這一任務。
  7. The attitude control system using reaction thrusters is studied. based on phase plane theory, pd control law, time - optimal control law and time - fuel optimal control law were designed. characteristics and application conditions of these laws were compared in simulations

    針對以噴氣推力器作為執行機構的姿態控制系統,基於相平面分析方法,分別設計了pd 、時間最優和燃料-時間混合最優控制律,在模擬中分別比較了這幾種方法的特點和適用條件。
  8. Microwave plasma thruster ( mpt ) is a new type of electro - thermal thruster, which has widely applied prospect because of its high specific impulse, long lifetime, low plume contaminant and so on

    微波等離子推力器( mpt )是一種新型的電熱型推力器,它具有比沖高、壽命長、羽流污染小等優點,具有廣闊的應用前景。
  9. Microwave plasma thruster ( mpt ) is studied in college of astronautics, northwestern polytechnical university and it is a new type of electro - thermal thruster. in order to study the performance of mpt more experiments must be taken, and an instant, exact and convenient system of measuring and controlling is very important in all of these experiments

    西北工業大學航天學院微波等離子推力器( mpt ? microwaveplasmathruster )研究需要通過大量的試驗探索mpt的各項性能,因此實時、準確、便捷的測控系統將為mpt的研製帶來極大的便利,深入開展測控技術的研究十分必要。
  10. Test results have shown that with discharge energy of 40 j, our ppt ' s thrust has reached more than 0. 605 mn, and its isp is 1188 s and weight is 4. 2kg, which reaches the level of current ppt used in the world

    所研製的脈沖等離子體推力器樣機質量為4 . 2kg ,在放電能量為40j時,為0 . 605mn ,比沖為1188s ,達到國際同期空間試驗樣機的水平。
  11. Parameter distributions within the thruster and its macroscopical performance were presented

    給出了不同集氣腔總壓下推力器內部參數分佈及其宏觀性能。
  12. Firstly, after the analysis of the specific hydrodynamic problem in detail, this thesis builds up an integrated simulation system of auv recovery

    首先,基於回收時特殊的流體動模型,構造了回收的集成模擬,包括水動模擬、推力器模擬以及海洋環境模擬等等。
  13. Development and key problems of laser plasma micro - thruster

    激光等離子體微推力器的發展及熱點問題
  14. Microwave plasma thruster ( mpt ) is a new studying type electro - thermal propulsive device. it has prospective application in spacecraft

    微波等離子推力器( microwaveplasmathruster ? mpt )是一種新型的在研電熱進裝置。
  15. Using gyro measurements during periods of thruster firing, with thruster outputs, mass property identification is achieved through recursive least squares algorithms on the basis of the refined dynamics equation. the approach addresses the issue by segmenting the problem into two sub - problems which both allow closed form solution to reduce computation load

    該方法利用衛星上的陀螺輸出和推力器控制指令作為演算法的輸入,在修正的衛星姿態動學模型基礎上,導了衛星質量特性在線辨識遞最小二乘演算法,將質心位置和轉動慣量矩陣的辨識解耦以降低辨識演算法的維數,減少計算量。
  16. Thruster - hull interaction

    推力器與船體相互影響
  17. When the propellant was lead styphnate and nickel hydrazine nitrate, their properties of ignition and thrust were investigated under different chamber diameter and different proportion of the mixed propellant. the influence of different thruster parameters on thruster properties was calculated

    研究了史蒂酚酸鉛和硝酸肼鎳在不同藥室直徑和藥劑配比下的點火和進性能,並且計算了推力器參數對性能的影響。
  18. To investigate effect of plenum chamber total pressure on arcjet thruster operation, numerical simulation of operation under various plenum chamber total pressures was performed on the basis of mechanism analysis on its operation and modeling for chemical non - equilibrium flow and steady state electromagnetic field within it

    摘要為了研究集氣腔總壓對電弧噴射推力器工作過程的影響,在分析其工作機理的基礎上採用化學非平衡流動和穩態電磁流體電磁場模型對不同集氣腔總壓下推力器工作過程進行了數值模擬。
  19. Thruster - current interaction

    推力器與水流相互影響
  20. Modularization methods are used to establish the mathematical models and simulation program for ship ' s dp systems. it included ship ' s moving models of low frequency moving and high frequency moving, thruster ' s models and environmental mathematical models ( wind, wave and current ). the models have been proved to be correct by simulation method

    利用模塊化思想研究了船舶動定位系統的數學模型、並且建立了模擬程序,包括船舶低頻運動模型、高頻運動模型、推力器模型和環境(風、海浪和海流)數學模型,通過模擬實驗驗證了模型的正確性。
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