Combustion mechanism of glycidyl azide polymer

被引:38
作者
Hori, K
Kimura, M
机构
[1] Minist Educ Culture & Sci, Inst Space & Astronaut Sci, Kanagawa 229, Japan
[2] NOF Corp, Taketoyo Plant, Taketoyo, Aichi 47023, Japan
关键词
D O I
10.1002/prep.19960210310
中图分类号
O69 [应用化学];
学科分类号
081704 ;
摘要
A combustion model of glycidyl azide polymer (GAP) is presented. Linear burning rate and temperature profile measurements of model samples led us to the conclusion that linear burning rate is controlled by N-2 liberation process below the pressure exponent break point (2.3 MPa). Further, scanning electron microscope (SEM) photographs and Fourier transform infrared (FTIR) spectra of quenched samples by rapid depressurization of the combustor show that the N-2 liberation process is strongly limited to the melt layer at the combustion surface and the profile of the heat release rate is probably delta -function like. This fact enables the application of an asymptotic analysis to this phenomenon.
引用
收藏
页码:160 / 165
页数:6
相关论文
共 11 条
[1]  
[Anonymous], PROPELL EXPLOS PYROT
[2]  
BUCKMASTER JD, 1982, THEORY LAMINAR FLAME, P13
[3]   THERMAL-DECOMPOSITION OF ENERGETIC MATERIALS .54. KINETICS AND NEAR-SURFACE PRODUCTS OF AZIDE POLYMERS AMMO, BAMO, AND GAP IN SIMULATED COMBUSTION [J].
CHEN, JK ;
BRILL, TB .
COMBUSTION AND FLAME, 1991, 87 (02) :157-168
[4]   MASS-SPECTROMETRIC KINETIC-STUDIES ON SEVERAL AZIDO POLYMERS [J].
FARBER, M ;
HARRIS, SP ;
SRIVASTAVA, RD .
COMBUSTION AND FLAME, 1984, 55 (02) :203-211
[5]   HISTORICAL DEVELOPMENT OF GLYCIDYL AZIDE POLYMER [J].
FRANKEL, MB ;
GRANT, LR ;
FLANAGAN, JE .
JOURNAL OF PROPULSION AND POWER, 1992, 8 (03) :560-563
[6]  
HELMY AM, 1987, 871725 AIAA
[7]   BURNING RATE CHARACTERISTICS OF GAP PROPELLANTS [J].
KUBOTA, N ;
SONOBE, T ;
YAMAMOTO, A ;
SHIMIZU, H .
JOURNAL OF PROPULSION AND POWER, 1990, 6 (06) :686-689
[8]  
MALUURA I, 1994, P ANN C JAPAN EXPL S, P73
[9]  
REID CR, 1977, PROPERTIES GASES LIQ, P524
[10]  
WILLIAMS FA, 1985, COMBUSTION THEORY, P155