The thermal decomposition characteristics of GAP simulated low oxygen fuel rich propellant were studied by using DSC method. The effect of TMO catalysts on the thermal decomposition characteristics is investigated in this paper.

 
  • 采用 DSC方法研究了 GAP模擬貧氧推進(jìn)劑的常壓熱分解特性 ,同時(shí)考察了 TMO催化劑對 GAP模擬貧氧推進(jìn)劑熱分解特性的影響。
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