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.

 
  • 為了認清固液火箭發(fā)動(dòng)機混合燃燒過(guò)程,采用熱平板導熱方式對固體燃料進(jìn)行熱分解實(shí)驗,得到了固體燃料的化學(xué)動(dòng)力學(xué)參數。
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