solid-liquid hybrid rocket

 
  • 固液混合火箭

solid-liquid hybrid rocket的用法和样例:

例句

  1. This paper mainly discusses available structures of the liquid hybrid bearings and the key technologies that need to be solved for the liquid rocket engine turbopump.
    针对液体火箭发动机涡轮泵特殊工作环境,讨论了流体动静压轴承可采用的结构形式和需要解决的关键技术。
  2. Chiaverini, M.J. et.Al., “Pyrolisis Behavior of Hybrid Rocket Solid Fuels Under Rapid Heating Conditions,” AIAA Paper No. 97-3078, 1997.
    施耿维;“混合推进剂燃烧组织与性能”;国立成功大学航空太空工程研究所硕士论文(1999).
  3. Altman D. Hybrid rocket development history. AIAA Paper 91-2515.
    单建胜等.;固液火箭发动机的研制及其应用
  4. Sound has to travel through solid liquid or air to reach our ears.
    声音必须通过固体液体或气体才能传到我们耳中。
  5. In order to know combustion process of hybrid rocket,pyrolysis test of solid fuel was carried out by using hot-plate heat conduction mode,then chemical kinetic parameters of solid fuel were obtained.
    为了认清固液火箭发动机混合燃烧过程,采用热平板导热方式对固体燃料进行热分解实验,得到了固体燃料的化学动力学参数。
  6. Estey Paul N, Whittinghill Geroge R. Hybrid rocket motors propellant selection alternative. AIAA Paper 92-3592.
    单建胜等.;固液火箭发动机的研制及其应用

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