By means of DSC and PDTA methods,the thermal decomposition characteristics of GAP model fuel-rich propellant and its ingredients at both 0.1 and 0.5 MPa were investigated.

• 采用差示扫描量热法(DSC)与高压差热分析法(PDTA)，系统研究了GAP贫氧推进剂中主要组分以及GAP模拟推进剂的常压与高压热分解特性。