推進劑藥柱 的英文怎麼說

中文拼音 [tuījìnyàozhù]
推進劑藥柱 英文
charge; propellant
  • : 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...
  • : 進構詞成分。
  • : 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...
  • : Ⅰ名詞1 (藥物) medicine; drug; remedy 2 (某些有化學作用的物質) certain chemicals Ⅱ動詞1 [書面...
  • 推進 : 1 (推動工作 使前進) push on; carry forward; advance; give impetus to 2 [軍事] move forward; dri...
  1. Interface debond between propellant and liner is a key form of failure of the structure integrity in the analysis of solid rocket motor

    在固體火箭發動機結構完整性分析中,襯層/推進劑藥柱粘接界面的脫粘是完整性被破壞的關鍵形式之一。
  2. 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。
  3. The mechanical properties of improved double-base propellants enabled one to envisage grain geometrics with large combustion areas and consequently high thrusts.

    經過改的雙基的機械性能使我們能夠指望獲得大燃燒面的幾何形狀,從而得到大力。
  4. The antiablation of silicone rubber liner can be improved both by changing the structure of unvulcanized rubber and adding antiablative fillers, and the bond strength between propellant charge and the liner would be increased largely by coating the primer liquid on the charge surface

    硅橡膠包覆層中填料的粒徑對硅橡膠的補強效果十分重要;可從改變生膠結構、添加耐燒蝕填料兩方面來改善硅橡膠包覆層的耐燒蝕性;在推進劑藥柱表面上塗覆底塗液可以大幅提高硅橡膠包覆層與的粘接強度。
  5. 4. in order to further improve and raise storage, energy and combustion properties of boron - based fuel - rich solid propellant, while the present slurries of boron - based fuel - rich solid propellant can be cast and cured to form defect - free propellant grain, ap grading and metal fuels changing including variety and addition amount have been adjusted and investigated. the result shows that, after the adjustment, all the slurries can be cast to obtain structural perfect propellant grain which may be used to test various propellant properties

    4 、為了使現有含硼的燃燒等性能一步提高和改善,同時為了能使現有含硼漿澆鑄后得到結構完整性和均勻性更好的,在2 、 3研究的基礎上,對ap的級配、低燃點金屬燃燒的品種和加入量等行了較深入的研究,結果表明:這些組分行調節后的各漿的流平性變化均能滿足澆鑄要求,並製成能其它性能測試的小方坯。
  6. Last, the result is compared with the result of analytic method. this paper provides a new method to analyze the grain structural integrality. the result provides the gist of grain figure in optimize design

    通過這些計算和分析,為底排?火箭彈助火箭推進劑藥柱結構完整性分析的有限元法提供參考,為形的優化設計提供依據。
  7. Solid rocket motor ( srm ) grain is casted integrally from solid propellants. it is one of the important structural components and also provides fuels for srm. the reliability of srm grain should be paid great attention

    固體火箭發動機是由固體整體澆鑄而成的,既為發動機提供燃料,又是重要的結構組成部分,其安全性不容忽視。
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