Menke K,Born M,Kempa P B. AN/PolyGLYN propellants-minimum smoke propellants with reduced sensitivity[C]∥37th International Annual Conference of ICT,Karlsruhe. 14,2006.
[2]
Khandhadia P S,Burns S P. Thermally stable nonazide automotive air-bag propellants: US 6306232[P]. 2001.
[3]
Hammerl A,Hiskey M A,Holl G,et al. Azidoformamidinium and guanidinium 5,5′-azotetrazolate salts[J]. Chem Mater,2005,17(14): 3784-3793.
[4]
Belov G V. Termodinamichesky analiz produktov sgoraniia pri vysokih davelniiah[C]∥Vestnik MGTU(Russia),1993,2: 43-46.
Ren Wu-zheng. Theoretic and Practice of Explosives and Pyrotechnics[M]. Beijing: China North Chemical Industries Corp. 2001: 259.
[7]
LIU Zi-ru,LIU Yan,FAN Xi-ping,et al. Thermal decomposition of RDX and HMX part Ⅰ: Characteristic values of thermal analysis[J]. Chinese Journal of Explosives and Propellants,2004,27(2): 63-66.
[8]
Lengell G,Izot A,Duteroue J,et al. Steady state burning of homogeneous propellants[M]∥Kuo Kenneth K,Summerfield Martin. Fundamental of Solid Propellants Combustion. Washington D C: AIAA,1984,Vol. 90,Chapter 7.
[9]
Singh H,Rao K R. Mechanism of combustion of catalyzed double base propellants[J]. Combustion and Flame,1988,71: 205.
[10]
Preckel R F. Plateau ballistics in nitrocellulose propellants[J]. AIAA Journal,1965,3(2): 346-347.
[11]
WANG Han,ZHAO Feng-qi,LI Shang-wen,et al. Function of carbon materials used in solid propellants and their action mechanism[J]. Chinese Journal of Explosives and Propellants,2006,29(4): 32-35.
[12]
WANG Jiang-ning. Studies on combustion disciplines of DB and CMDB propellants with catalysts[D]. Beijing: Beijing Institute of Technology,2004.
[13]
Helmy A M,Selph T M,Hollister. GAP propellant for gas generator application[R]. AIAA-87-1725,1987.
[14]
Raman K V,Singh H. Ballistic modification of RDX-CMDB propellants[J]. Propellant,Explosive and Pyrotechnic,1988,13: 149-151.
[15]
Menke K,Gunser G,Schnoering M,et al. Burning rate enhancement of AN-propellants by TAGN and GZT[C]∥34th International Annual Conference of ICT,Karlsruhe. 22,2003.
[16]
Menke K,Gunser G,Bohnlein J,et al. Combustion modification of AN propellants with energetic binders by TAGN and GZT[C]∥9-IWCP Workshop on Combustion and Propulsion,Lerici,Italy,2003.
[17]
Sivabalan R,Talawar M B,Senthilkumar N,et al. Studies on azotetrazolate based high nitrogen content high energy materials potential additives for rocket propellants[J]. J Therm Anal Cal,2004,78: 781-792.
[18]
Bucerius K M,Eisenreich N,Schmid H,et al. Gas generating mixture containing copper diammine dinitrate: US5663524[P]. 1997.