Thermal decomposition of NEPE propellant containing hexanitrohexaazisowurtzita(HNIW) was investigated by thermogravimetry(TG) and differential scanning calorimetry(DSC).

• 利用TG和DSC研究了含六硝基六氮杂异伍兹烷(HNIW)的NEPE推进剂的热分解特性。