推进剂药柱的英文

• charge; propellant
• propellant grain
• propellant stick

• "推进剂"英文翻译    propellant; propellent; prop ...
• "药"英文翻译    medicine; drug; remedy
• "固体推进剂药柱" 英文翻译 :    solid-propellant grain
• "火箭推进剂药柱组" 英文翻译 :    rocket propellant charge assembly
• "十字形固体推进剂药柱" 英文翻译 :    cruciform solid-propellant grain
• "实心固体推进剂药柱" 英文翻译 :    solid-propellant rod
• "浇铸成型的固体推进剂药柱" 英文翻译 :    castable solid-propellant grain
• "星状药柱推进剂" 英文翻译 :    star grain propellant
• "氧化剂药柱" 英文翻译 :    oxidizer grain
• "固液推进剂固体药柱" 英文翻译 :    hybrid solid grain; hybrid-fuel grain
• "固体燃烧剂药柱" 英文翻译 :    solid-fuel grain
• "固体氧化剂药柱" 英文翻译 :    solid-oxidizer grain
• "推进剂" 英文翻译 :    propellant; propellent; propulser; propulsive agent
• "推进剂；推进的" 英文翻译 :    propellant
• "安全推进剂" 英文翻译 :    safe propeller
• "板状推进剂" 英文翻译 :    sheet propeller
• "爆燃推进剂" 英文翻译 :    deflagrating propeller
• "倍基推进剂" 英文翻译 :    double-based propellant
• "超冷推进剂" 英文翻译 :    hydrogen propeller
• "触变推进剂" 英文翻译 :    thixotropic propellant
• "单基推进剂" 英文翻译 :    simple-base propeller; single-base propellants
• "单元推进剂" 英文翻译 :    katergol; mono propellant; monopropellant; self-contained propeller
• "单质推进剂" 英文翻译 :    monopropellant
• "导弹推进剂" 英文翻译 :    missile propeller
• "低能推进剂" 英文翻译 :    low-energy propeller

• Interface debond between propellant and liner is a key form of failure of the structure integrity in the analysis of solid rocket motor
  在固体火箭发动机结构完整性分析中,衬层/推进剂药柱粘接界面的脱粘是完整性被破坏的关键形式之一。
• 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
  通过这些计算和分析，为底排?火箭弹助推火箭推进剂药柱结构完整性分析的有限元法提供参考，为药柱药形的优化设计提供依据。
• 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
  硅橡胶包覆层中填料的粒径对硅橡胶的补强效果十分重要；可从改变生胶结构、添加耐烧蚀填料两方面来改善硅橡胶包覆层的耐烧蚀性；在推进剂药柱表面上涂覆底涂液可以大幅提高硅橡胶包覆层与推进剂的粘接强度。
• 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
  由于固体火箭发动机的推进剂药柱是一种粘弹性材料,衬层和绝热层也具有粘弹性性质,因此其界面脱粘问题实际上是弹性-粘弹性或双粘弹性各向同性材料界面裂纹问题,对该问题的研究涉及到粘弹性力学、界面断裂力学和燃烧学等相关学科。