推進劑特性 的英文怎麼說

中文拼音 [tuījìnjìtèxìng]
推進劑特性 英文
propellant characteristic
  • 推 : 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...
  • 進 : 進構詞成分。
  • 劑 : Ⅰ名詞1 （藥劑; 制劑） a pharmaceutical or other chemical preparation 2 （某些有化學作用的物品） a...
  • 特 : Ⅰ形容詞（特殊; 超出一般） particular; special; exceptional; unusual Ⅱ副詞1 （特別） especially; v...
  • 性 : Ⅰ名詞1 （性格） nature; character; disposition 2 （性能; 性質） property; quality 3 （性別） sex ...
  • 推進 : 1 （推動工作 使前進） push on; carry forward; advance; give impetus to 2 [軍事] move forward; dri...
  • 特性 : characteristic（s）; character; performance; features; properties; behaviour; response; character...
  1. This includes both the fundamental bending characteristics of the airframes and the propellant dynamics.

    這包括飛行器結構的基本彎曲特性和推進劑動力學。
  2. Flame temperature measurements can be used as a guide in discussing energetics of a homogeneous propellant.

    火焰溫度的測定可作為討論均質推進劑能量特性的指導。
  3. Space systems - fluid characteristics - kerosene propellant

    航天系統.流體特性.煤油推進劑
  4. Space systems - fluid characteristics - nitrogen tetroxide propellant

    航天系統.流體特性.四氧化氮推進劑
  5. Aerospace series - space systems - fluid characteristics, sampling and test methods - nitrogen tetroxide propellants

    航空航天系統.航天系統.流體特性抽樣和試驗方法.四氧化氮推進劑
  6. What the study of the software of configuration analysis of liquid propellant space propulsion systems solved is how to develop the software of configuration analysis of liquid propellant space propulsion systems using scientific software model based on the characteristics of liquid propellant space propulsion systems in order to improve the performance and reduce the mass etc. it ' s important that can save fees and improve corporation ' s ability of participating competition

    液體推進劑空間推進系統構型分析軟體研究所要解決的問題是如何根據液體推進劑空間推進系統的特點，通過運用科學的軟體模型開發液體推進劑空間推進系統構型分析軟體。其目的是為了提高推進系統性能、減少推進系統質量等。進行液體推進劑空間推進系統構型分析軟體研究對于節約國家經費、提高企業競爭力有著重要的意義。
  7. Explosives for civil uses - propellants and rocket propellants - determination of properties of black powder

    民用爆炸物.推進劑和火箭推進劑.黑火藥特性的測定
  8. Space systems - fluid characteristics - hydrazine propellant

    航天系統.流體特性.聯氨推進劑
  9. Especially, when - bi together with a little carbon black ( cb ) or copper salt is used, the catalytic effect is better ; the flame structures of the double - base propellants containing - bi are similar to the typical plateau double - base propellant, but the combustion temperature distribution has been changed because of adding the - bi ; and the active components of catalysts deposit on the burning surface of propellants and the quenched surfaces of propellants with various catalysts possess different structure

    它與銅鹽和少量炭黑（ cb ）復合后，催化效果更優； 2 ， 4 -二羥基苯甲酸鉍加入后，推進劑的火焰結構保持了典型平臺雙基推進劑的結構特徵，但改變了雙基推進劑燃燒波溫度分佈，炭黑和銅鹽的加入對2 ， 4 -二羥基苯甲酸鉍的催化作用有很大影響；催化劑分解的活性組分富集在燃燒表面，不同催化劑使推進劑熄火表面形成不同的結構。
  10. Boron coated with different content ap on the rheological properties of the slurry containing 30 % boron have been carried out with the help of the sv2 / sv2fl measuring system in haake rotary viscometer. the experimental results reveal that the rheological properties of the slurry of boron coated with 20 % ap is best, namely, the slurry has a good levelability and a long pot life. the optimum conditions in the preparation of the boron - based propellant with 30 % boron in weight were obtained, and a technical and theoretical foundation has been established for the formulae determination

    3 、用進口haake旋轉粘度儀對不同包覆硼粉在硼含量為30以上的實驗配方藥漿中的流變特性研究，篩選出用20 ap包覆的硼粉所製成的藥漿不僅流平性好而且適用期長，同時找到了含硼量為30的高含硼量推進劑藥漿成功研製的成熟工藝過程及條件，為配方的進一步定型奠定了較扎實的技術和理論基礎。
  11. As to the experimental study, a test system was designed firstly, which include propellant feed system, cooling system, controlling system and measure system. secondly, a test engine was designed according to the experimental requirement. on this basis, experiments under different working conditions were done, and the results of them were analyzed, which showed the combustion efficiency and stability

    實驗方面，首先設計了針對三組元發動機推力室工作過程進行試驗的試驗系統，包括推進劑供應系統與冷卻水供應系統、控制系統以及壓力、溫度、流量的測量採集系統；其次，設計出符合試驗要求的縮尺發動機；最後針對所設計的試驗系統和發動機，進行了不同工況的試驗，對所得數據進行了分析處理，得到了不同工況下燃燒效率和燃燒穩定性特性。
  12. Space systems - fluid characteristics - hydrogen propellant

    航天系統.流體特性.氫推進劑
  13. It is very difficult to research the burning characteristic of high energy propellant in the ddt pipe applying the ionization probe. but the satisfactory results can be easily got using photoelectricity triode

    用探針法研究ddt管中高能推進劑的燃燒波和爆轟波的傳播特性，因各種因素的影響難以得到滿意的結果，用光電三極體代替電離探針可得到相對理想的結果。
  14. Aerospace series - space systems - fluid characteristics, sampling and test methods - monomethylhydrazine propellant

    航空航天系統.航天系統.流體特性抽樣和試驗方法.單甲基肼推進劑
  15. Energetic materials for defense. physico - chemical analysis and properties. graphite, carbon black, tin oxide of single and double base properlants

    國防用高能材料.物理-化學分析及特性.單基和雙基推進劑的石墨碳黑和氧化錫
  16. On adjusting function components for optimizing rheological properties of slurry of boron - based fuel - rich solid propellant

    功能組分對含硼富燃固體推進劑藥漿流變特性的影響
  17. Aerospace series - space systems - fluid characteristics, sampling and test methods - kerosine propellant

    航空航天系統.航天系統.流體特性抽樣和試驗方法.煤油推進劑
  18. It is concluded that increase of temperature in csp matrix is of great extent, and is in dependence with impact velocity, rate of deformation and thermorheologic

    分析計算表明:撞擊變形條件下粘性加熱使推進劑基體溫度顯著上升，溫度升幅與撞擊速度、剪切變形、推進劑熱流變特性密切相關。
  19. The dynamic aspects of the combustion process are determined primarily by the injection pattern, the propellant combination, and the operating conditions.

    燃燒過程的動力特性主要由噴射型式，推進劑組合及工作條件來確定。
  20. The experiment research of the energy characteristics of the solid propellant of the over - storage solid rocket motors

    超期貯存發動機固體推進劑能量特性試驗研究
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