Fabrication and thermal decomposition of glycidyl azide polymer modified nitrocellulose double base propellants  被引量:2

Fabrication and thermal decomposition of glycidyl azide polymer modified nitrocellulose double base propellants

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作  者:Benbo Zhao Tianfu Zhang Zhen Ge Yunjun Luo 

机构地区:[1]School of Materials Science and Engineering, Beijing Institute of Technology

出  处:《Science China Chemistry》2016年第4期472-477,共6页中国科学(化学英文版)

摘  要:Glycidyl azide polymer (GAP) with the advantages of non-volatility and excellent thermal stability is a candidate as a re- placement for nitroglycerine (NG) in a double base propellant. The GAP-NC double base propellants were formulated with GAP and nitrocellulose (NC) fibers. Tensile test and SEM characterization indicated that GAP-NC propellants had a homoge- neous structure. Thermogravimetric analysis of GAP-NC propellants revealed that the onset decomposition temperature reached a high level ranging from 192.9 to 194.6 ℃, which indicated that the substitution of NG with GAP contributed to the safe storage and process operations for double base propellant. The result analysis of decomposition products of GAP-NC propellants showed that the main gas decomposition products of the propellants were NO, NO〉 CO, CO2, NH3, CH4, HCN, N2 CH20 and C2H40. The thermal decomposition process of the specimens was proposed.Glycidyl azide polymer(GAP) with the advantages of non-volatility and excellent thermal stability is a candidate as a replacement for nitroglycerine(NG) in a double base propellant. The GAP-NC double base propellants were formulated with GAP and nitrocellulose(NC) fibers. Tensile test and SEM characterization indicated that GAP-NC propellants had a homogeneous structure. Thermogravimetric analysis of GAP-NC propellants revealed that the onset decomposition temperature reached a high level ranging from 192.9 to 194.6 °C, which indicated that the substitution of NG with GAP contributed to the safe storage and process operations for double base propellant. The result analysis of decomposition products of GAP-NC propellants showed that the main gas decomposition products of the propellants were NO, NO_2, CO, CO_2, NH_3, CH_4, HCN, N_2, CH_2O and C_2H_4O. The thermal decomposition process of the specimens was proposed.

关 键 词:glycidyl azide polymers (GAP) NITROCELLULOSE double base propellant NITROGLYCERINE thermal decomposition 

分 类 号:V512.2[航空宇航科学与技术—航空宇航推进理论与工程]

 

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