Kuwahara T, Shinozasi N. Burning mechanism of ammonium nitrate/aluminum composite propellants[J].Journal of the Industrial Explosives Society,1992,53(3):131-136.
[2]
Kato K, Nakasita G. Burning rate characteristics of GAP/AN propellants[J].Journal of the Japan Explosives Society,1995,56(3):130-134.
Klaus Menke, Jutta B(O) hnlein-Mauβ, Hiltmar Schubert. Characteristic properties of AN/GAP-propellants [J].Propellants,Explosives,Pyrotechnics,1996, 21:139-145.
[5]
Yoshio Oyumi, Eishu Kimura. Insensitive munitions(IM) and combustion characteristics of GAP/AN composite propellants [J].Propellants,Explosives,Pyrotechnics,1996,21:271-275.
[6]
赵孝彬, 张小平, 侯林法. GAP/AN推进剂的热分解催化研究[J].固体火箭技术,1999,22(1):46-49.ZHAO Xiao-bin, ZHANG Xiao-ping, HOU Lin-fa. Study of thermal decomposition catalytic of GAP/AN propellant[J].Journal of Solid Rocket Technology,1999,22(1):46-49.
[7]
张杰,杨荣杰. 六硝基六氮杂异兹烷的燃烧和催化热分解研究 [J].兵工学报,2003,24(4):455-458.ZHANG Jie, YANG Rong-jie. Study on catalyst combustion and thermal decomposition of hexanitrohexaazai-sowurtzitane[J].Acta Armamentarii:2003,24(4):455-458.
[8]
Kuwahara T, Matsuo S. Burning rate characteristics and ignition characteristics of ammonium nitrate/ammonium perchlorate composite propellants[J].Journal of the Japan Explosives Society,1995,56(3):135-140.
[9]
Kazita Y, Saito T, Yamaya T, et al. Ignition characteristics of GAP/AN/AP-based solid propellants for low pollution at sub-atmospheric pressures[J].Journal of the Japan Explosives Society,1996,57(1):1-8.