Thermal decomposition of HTPB/AP and HTPB/HMX mixtures with low content of oxidizer

Journal of Thermal Analysis and Calorimetry

Volumn 119, Issue 3, 2015, Pages 1673-1678

  Wang, Ying Hong ^a   Liu, Lin Lin ^a   Xiao, Lian Yi ^a   Wang, Ze Xu ^a  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

Author keywords

AP; Fuel rich propellant; HMX; HTPB; Thermal decomposition

Indexed keywords

COMBUSTION; DECOMPOSITION; EXPLOSIVES; FUELS; HMX; INORGANIC COMPOUNDS; MIXTURES; OXYGEN; POLYBUTADIENES; PROPELLANTS; PYROLYSIS;

AP; COMBUSTION PERFORMANCE; COMBUSTION TEMPERATURES; FUEL-RICH PROPELLANT; HTPB; HYDROXYL-TERMINATED POLYBUTADIENE; INERT ATMOSPHERES; THERMAL DECOMPOSITION PROCESS;

HTPB PROPELLANTS;

EID: 84925465071     PISSN: 13886150     EISSN: None     Source Type: Journal    
DOI: 10.1007/s10973-014-4324-z     Document Type: Article

References (16)

1. Kuo KK, Summerfield M. Fundamentals of solid-propellant combustion. New York: American Institute of Aeronautics and Astronautics; 1984.
2. Cai WD, Thakre P, Yang V. A model of Ap/Htpb composite propellant combustion in rocket-motor environments. Combust Sci Technol. 2008;180(12):2143-69. doi: 10.1080/00102200802414915.
3. Chen JK, Brill TB. Chemistry and kinetics of hydroxyl-terminated polybutadiene (Htpb) and diisocyanate Htpb polymers during slow decomposition and combustion-like conditions. Combust Flame. 1991;87(3-4):217-32. doi: 10.1016/0010-2180(91)90109-O.
4. Du TF. Thermal-decomposition studies of solid-propellant binder Htpb. Thermochim Acta. 1989;138(2):189-97.
5. Bircumshaw LL, Newman BH. The thermal decomposition of ammonium perchlorate.2. the kinetics of the decomposition, the effect of particle size, and discussion of results. Proc R Soc Lon Ser-A. 1955;227(1169):228-41. doi: 10.1098/rspa.1955.0006.
6. Bircumshaw LL, Phillips TR. The kinetics of the thermal decomposition of ammonium perchlorate. J Chem Soc. 1957;. doi: 10.1039/Jr9570004741.
7. Boldyrev VV. Thermal decomposition of ammonium perchlorate. Thermochim Acta. 2006;443(1):1-36. doi: 10.1016/j.tca.2005.11.038.
8. Menke K, Eisele S. Rocket propellants with reduced smoke and high burning rates. Propell Explos Pyrot. 1997;22(3):112-9. doi: 10.1002/prep.19970220304.
9. Liu L-L, He G-Q, Wang Y-H. Thermal reaction characteristics of the boron used in the fuel-rich propellant. J Therm Anal Calorim. 2013;114(3):1057-68.
10. Kaser F, Bohn MA. Decomposition in HTPB bonded HMX followed by heat generation rate and chemiluminescence. J Therm Anal Calorim. 2009;96(3):687-95. doi: 10.1007/s10973-009-0031-6.
11. Rocco JAFF, Lima JES, Frutuoso AG, Iha K, Ionashiro M, Matos JR, et al. Thermal degradation of a composite solid propellant examined by DSC-kinetic study. J Therm Anal Calorim. 2004;75(2):551-7. doi: 10.1023/B:Jtan.0000027145.14854.F0.
12. Vyazovkin S, Wight CA. Kinetics of thermal decomposition of cubic ammonium perchlorate. Chem Mater. 1999;11(11):3386-93. doi: 10.1021/Cm9904382.
13. Li X, Liu X, Cheng Y, Li Y, Mei X. Thermal decomposition properties of double-base propellant and ammonium perchlorate. J Therm Anal Calorim. 2014;115(1):887-94.
14. Zhu Y-L, Huang H, Ren H, Jiao Q-J. Kinetics of thermal decomposition of ammonium perchlorate by TG/DSC-MS-FTIR. J Energ Mater. 2014;32(1):16-26.
15. Liu LL, He GQ, Wang YH. Effect of oxidizer on the combustion performance of boron-based fuel-rich propellant. J Propul Power. 2014;30(2):285-9. doi: 10.2514/1.B34909.
16. Liu LL, He GQ, Wang YH, Liu PJ. Factors affecting the measurement of the percentage of gaseous products from boron-based fuel-rich propellants. Cent Eur J Energ Mat. 2014;11(1):15-29.