Skip to main content
ACS Omega logoLink to ACS Omega
. 2021 Jan 14;6(3):2025–2033. doi: 10.1021/acsomega.0c04985

Mechanism of Two Typical Binders BR and F2604 on Thermal Decomposition of HMX

Wanxiao Guo 1, Yaning Li 1, Wei Xiao 1, Jian Li 1, Zhiwei Han 1, Boliang Wang 1,*
PMCID: PMC7841798  PMID: 33521441

Abstract

graphic file with name ao0c04985_0011.jpg

DSC–TG–FTIR–MS coupling technology was used to study the mechanism of two typical binders, that is, BR and F2604, on the thermal decomposition behavior of the HMX crystal. The results show that both BR and F2604 can induce premature decomposition of HMX and increase the activation energy of HMX. Especially in the case of HMX/BR particles, the decomposition temperature is the lowest, but the activation energy is the highest. Based on the results of DSC–TG–FTIR–MS, it is found that the rapid mechanism of binder and active intermediate products inhibits the reaction of relatively inert intermediate products and prolongs the continuous generation time of gas products in the composite particles, which delays the decomposition of HMX to a certain extent. This study is helpful for us to better understand the thermal decomposition behavior of HMX composite particles and provides reference for the application of high-energy composites.

1. Introduction

With the continuous development of weapon systems, modern warfare has developed from the previous one-way direct damage strike to the complex system confrontation combining penetration defense and strike bunkers. The combat mode is presented in a more and more multi-dimensional manner. Because of the deterioration of the battlefield environment, a large part of the loss of weapons and ammunition comes from the self-explosion of ammunition caused by accidental ignition, which in turn leads to disastrous consequences for combat platforms such as ships.1 Therefore, ammunition in modern weapon systems is expected to have not only higher damage power but also higher reliability and safety when it is impacted by unexpected external dangerous stimuli.2,3 Therefore, mixed insensitive explosives, represented by polymer-bonded explosives (PBX) explosives, are gradually emerging.47

PBX explosives are mainly composed of high-energy density energetic materials and polymer binders. High-energy density energetic materials include RDX, HMX, CL-20, and so forth, which have high energy but sensitive to external stimuli.810 The polymer binder including C–H-based polymers, such as HTPB and BR, and C–F-based fluoropolymer, such as Viton A, have been developed for PBX and propellant formulations.7,1115 Binder, as an indispensable component of insensitive explosives, provides PBX with good mechanical properties and good safety. However, because of various heterogeneous decomposition reactions in PBX explosives, the solid–state reaction of high-energy composite materials is very complex, and the decomposition reaction mechanism is also be affected by a very small amount of polymer matrix.1620 Therefore, studying the thermal decomposition behavior and kinetics of composite explosives is an essential part to evaluate the safety performance.2124

The thermal decomposition behavior and kinetics of HMX-based PBX have been extensively studied through non-isothermal thermogravimetry (TGA) or differential scanning calorimetry (DSC).2534 In the published literature, more attention has been paid on the thermal decomposition behavior and kinetics of PBX based on HMX mixed with a binder, yet fewer articles focus on different reaction mechanisms caused by the basic reaction between binder and HMX. Wu et al.35 studied the thermal decomposition behavior of CL-20/HMX eutectic with nano-Fe2O3 and rGO-Fe2O3 by DSC–TG–MS–FTIR coupling technology and proposed the thermal decomposition mechanism of CL-20/HMX eutectic. Lalit et al.36 used TGA and CRT combined with FTIR to obtain the mole fraction distribution of gas decomposition products evolved from liquid-phase HMX and studied the basic liquid-phase reaction combining with quantum mechanical calculation. Studying the decomposition mechanism of composite high-energy materials can provide a better understanding of its thermodynamic behavior and more fundamental mechanism research for composite high-energy materials.37,38

In this paper, we study the effects of two typical binders BR and F2604 on the thermal decomposition of HMX. The kinetic parameter activation energy of HMX and composite materials is calculated by the Kissinger method based on DSC data, and the kinetic model of the sample was analyzed by the Malek method. The DSC–TG–MS–FTIR coupling technology is used to test the evolution process of gas products in the thermal decomposition process. Based on the analysis of the thermal decomposition process and gas products of HMX, the action mechanism of BR and F2604 is proposed, which provided a reference for the application of the two binders in HMX-based explosives.

2. Materials and Experimental Section

2.1. Materials

HMX was purchased from Gansu Yinguang Chemical Industry Group Co., Ltd. (Baiyin, Gansu, China) cis-1,4-polybutadiene (BR, density is 0.91 g/cm3, and the relative molecular weight is 50,000–70,000) and fluoropolymer (F2604, density is 1.80 g/cm3, and the relative molecular weight is 150,000–200,000) were all industrially produced. The molecular structure is shown in Figure 1.

Figure 1.

Figure 1

Molecular structure of HMX, BR, F2604

2.1.1. Preparation of Composite Particles

The binder and HMX were weighed according to the mass ratio of 5:95. HMX was mixed in water and stirred, and the binder was dissolved in a low boiling point organic solvent, which is not miscible with water. Then, the binder solution was poured into the HMX aqueous solution, which was stirred violently, and the solvent was removed by distillation under continuous stirring. HMX-based composite particles were obtained after filtration. The detailed sample preparation process of HMX/BR is shown in Figure 2. The preparation process of HMX/F was similar, where only ethyl acetate was used to replace petroleum ether. For convenience, the composite particles were named HMX/BR and HMX/F. In the supporting documents, Figure S1 shows that the two binders are uniformly coated on the surface of the HMX crystal, and the FTIR results of Figure S2 indicate that there is only a certain physical interaction between the binder and HMX at room temperature.

Figure 2.

Figure 2

Preparation of HMX/BR composite particles.

2.2. Experimental Section

The DSC (NETZSCH DSC 204 F1 Phoenix, Germany) differential scanning calorimeter was used to test the thermal decomposition performance of energetic materials under Argon atmosphere. The sample weight was about 0.7 mg, and the heating rate was 5, 10, 15, and 20 K·min–1. The TGA-DSC3+ (METTLER TOLEDO)-FTIR (Nicolet iS50-GC/MS (Agilent 7890B-5977B) coupling technology was used for decomposition mechanism analysis; the sample mass was about 1 mg; Argon atmosphere and heating rate were with 10 K·min–1.

Figure 3 shows the DSC curves of pure HMX crystal and composite particles of HMX/BR and HMX/F at different heating rates. When the heating rate is 5 K min–1, the exothermic peaks of the pure HMX crystal, HMX/BR, and HMX/F in DSC curves are 277.9, 268.8, and 274.3 °C, respectively. BR and F2604 reduced the thermal decomposition peak of pure HMX from 277.9 to 268.8 and 274.3 °C, respectively. At the heating rates of 10, 15, and 20 K min–1, a similar reduction effect is also shown. The results indicated that both binders have an induction effect on the thermal decomposition of HMX, and the induction effect of BR is obvious. Figure. S2 shows the DSC curves of pure BR and F2604 at a heating rate of 10 K min–1. It can be seen that the decomposition temperatures of BR and F2604 are 373.8 and 488.6 °C respectively, which is higher than the decomposition temperatures of HMX. Therefore, we inferred that the chemical reaction of BR and F2604 with the HMX decomposition products induced the decomposition of HMX. In particular, BR with a long C–H chain has a strong adsorption effect on H and O ions, which induces O and H to separate from HMX molecules and react with them.

Figure 3.

Figure 3

DSC curves at various heating rates for (a) pure HMX, (b) HMX/BR, and (c) HMX/F.

3. Results and Discussion

3.1. Thermal Decomposition Behaviors

The effect of binder on the non-isothermal thermal decomposition kinetics of HMX is studied by Kissinger equation which can be expressed as

3.1. 1

In these equations, Ea is the activation energy, A is the pre-exponential factor, β is the heating rate, R is the ideal gas constant, and Tp is the peak temperature.

The calculated results of kinetic parameters are shown in Table 1. Compared with pure HMX, the addition of BR and F2604 increased Ea of HMX from 338.9 to 497.5 kJ mol–1 and 396.0 kJ mol–1, respectively, which means that the two binders could inhibit the thermal decomposition of HMX. The higher activation energy of HMX/BR indicates that the inhibition effect of BR is more obvious than that of F2604. In addition, we use AKTS software to analyze the DSC results and draw the T–α curve, as shown in Figure S4. The reaction rate was calculated according to the T–α curve, and the kinetic models of the three samples at a heating rate of 10 K/min were analyzed by the Malek method.4143 As shown in Figure 4, it can be seen that the kinetic models of the three samples are most similar to curves 39 and 40. Therefore, the kinetic models of HMX and its composite particles are f(α) = α/2 or f(α) = α, which follows the exponential rule. Generally, DSC results showed that BR and F2604 could reduce the decomposition temperature of HMX and induce HMX to decompose earlier; however, with the decomposition process, it gradually shows the inhibition effect on HMX decomposition.

Table 1. Pyrolysis Kinetics Parameters of HMX, HMX/BR, and HMX/F.

sample β/K·min–1 Tp/°C Ea/kJ·mol–1 lnA/s–1 r2
HMX 5 277.9 338.9 80.0 0.987
  10 281.6      
  15 285.1      
  20 288.2      
HMX/BR 5 268.8 497.5 116.7 0.998
  10 272.5      
  15 274.1      
  20 275.7      
HMX/F 5 274.3 396.0 93.1 0.988
  10 278.3      
  15 280.1      
  20 283.3      

Figure 4.

Figure 4

Comparison of the sample kinetic model obtained by the kinetic analysis method with the ideal model of the Malek method.

3.2. DSC–TG–FTIR–MS Results

To further understand the influence of two binders on the thermal decomposition of HMX, we investigated the thermal decomposition process of three particles at a heating rate of 10 K min–1 by DSC–TG–FTIR–MS coupling technology. The DSC–TG results are shown in Figure S5, and the DSC test is similar to the results in Section 3.1, which will not be discussed here. The TG results show that the mass decay of HMX/BR and HMX/F particles is faster than that of pure HMX, and that of the HMX/BR is the fastest, which means that both BR and F2604 binders can accelerate the conversion of HMX to gaseous products. At the same time, FTIR is used to detect the gas products generated during the thermal decomposition of high-energy particles. The infrared spectrum is shown in Figure 5a. The results revealed that the main decomposition gas products of HMX are CO2 (715 and 2310 cm–1), CHN (760 and 3315 cm–1), N2O (1285, 2220 and 2550 cm–1), NO2 (1550 cm–1), CH2O (1745 and 2802 cm–1), NO (1910 cm–1), and H2O (3500 cm–1), and more CO2 is produced with the addition of BR and F2604. In the infrared spectrum detection, CO has a relatively small dipole moment and N2 has a symmetrical structure and no dipole moment. Therefore, CO and N2 signals are not detected in the FTIR test.

Figure 5.

Figure 5

FTIR spectrum of the evolved gases at 280 °C.

During the thermal decomposition of HMX, we extracted the gas products at multiple time points in FTIR detection, as shown in Figures 6, S6 and S7, in which the red arrow indicates the appearance of the products and the black arrow indicates the disappearance of the products. The infrared spectrum of pure HMX showed that N2O (20 min) is the first gas product, followed by trace CO2 (21 min) and CHN (22 min), and then other gas products (NO2, NO, CH2O, H2O, and NO) appeared simultaneously in the infrared detection at 22.5 min. Figure S6 shows that when BR is added into HMX, some gas products will appear earlier, such as CHN (21.5 min), NO2, NO, CH2O, H2O, and NO (22 min), while Figure S7 shows that the formation time of gas products of HMX/F particles is similar to that of the pure HMX crystal. With the progress of the decomposition reaction, the infrared results show that the gas products of pure HMX, except N2O, almost disappear at about 24.5 min, while the disappearance time of HMX/BR and HMX/F gas products is about 26 and 27 min, respectively. Obviously, the addition of both binders prolonged the duration of gas product formation. Therefore, the FTIR results can be summarized as follows: BR induces HMX to decompose in advance and prolong the continuous formation time of gas products, while F does not show an obvious induction effect, but also prolong the continuous formation time of gas products.

Figure 6.

Figure 6

Evolution of gas products with decomposition time of the pure HMX crystal.

The gas chromatography–mass spectrometer (GC–MS) is used to further detect the composition and content of gas products, and the total particle flow spectrum is shown in Figure 7. Pure HMX showed strong ion flow peaks at 1.92, 2.55, 2.77, and 8.7 min and weak ion peaks at 11.5 and 14.5 min; because of the variety of HMX gas products, only fragments with relative ion flow intensity greater than 3% are selected for mass-core ratio (m/z) analysis. The mass spectrum corresponding to each ion flow peak is shown in Figure 8, and the possible structures corresponding to m/z are listed in Table 2. In the ion flow of 1.92 min, the main values of m/z are 14, 16, 28, 32, and 40; the corresponding fragments are CH2N2+, O+, CO, N2, O2, and CN2, respectively. Figure 8a shows that the addition of BR and F2604 increased the contents of CO, N2, and CH2N2+ and decreased the contents of O+, O2, and CN2, which means that the binder could promote some oxygen-containing reactions and generate stable products CO and N2. Figure 7 shows that the m/z of the fragment corresponding to 2.55 min is 44, and there is only one relatively stable fragment corresponding to CO2, while the m/z corresponding to 2.77 min is 30 and 44, and the corresponding product fragments are CH2O and N2O, respectively, which can be produced by further pyrolysis of intermediate products CH2N2O2. Moreover, Figure 7 shows that the relative ion flow peak values corresponding to 2.55 and 2.77 min are HMX/BR > HMX/F > HMX, which means that BR and F2604 promote the production of CO2, CH2O, and N2O.

Figure 7.

Figure 7

GC–MS spectrum of the evolved gases at 280 °C.

Figure 8.

Figure 8

Mass-nucleus ratio corresponding to ion flow in the MS spectrum (a) 1.92 min, (b) 2.55 min, (c) 2.77 min, and (d) 8.7 min.

Table 2. Possible Structure of Gaseous Products Detected by MS at 280 °C.

m/z 14 16 17 18 26 27 28 30 32 40 44 52 53 54 81
probable structures CH2N2+ O+ OH+ H2O CHCH, <CN+ CHN CO,N2, CH2N NO, CH2O O2 CN2 CO2, N2O C4H4 C2N2H C2N2H2 C3N3H3

For the weaker ion flow, the mass spectra of the composite particles and pure HMX are obviously different. At 11.5 min, the main m/z are 26, 27, and 28, and the corresponding main ion fragments are CHN and its isotopic ions CN and CH2N. The slightly higher ion flow peak in Figure 7 and the more fragments with m/z of 27 in Figure S8a indicate that the presence of BR and F2604 will promote the formation of CHN. In the 14.5 min ion flow peak, the main product fragments are CHN, CH2N, C2N2H, C2N2H2, C3N3H3, and so forth, of which CH2N is the CHN isotope, C2N2H is the C2N2H2 isotope, and C2N2H, C2N2H2, and C3N3H3 are products of group rearrangement. Figure S8b shows more CHN, CH2N rearrangement in HMX/BR and HMX/F to produce rearranged ions of C2N2H, C2N2H2, and C3N3H3. It is worth noting that among the three materials, only HMX/BR composite particles have an ion flow peak of 9.5 min, as shown in Figure S9, and the main fragments corresponding to the m/z are C4H4 and C2H2 indicate that BR has undergone fracture decomposition. No typical fluorine-containing fragment HF is detected in HMX/F particles, which may be because the F2604 has not been completely decomposed into HF or HF fragment quickly participates in the reaction, so it is not detected in the GC–MS test.

3.3. Thermal Decomposition Mechanism

During the thermal decomposition of HMX, the initial decomposition of HMX and the rapid oxidation mechanism in the decomposition process determine the thermal decomposition process of HMX.40 The thermal decomposition process of HMX mainly includes the breakage of the N–N bond, the separation of H and O, the fission of C–N ring, and the rapid oxidation of sensitive intermediate products into stable gas products. In this paper, the coupling analysis of DSC–TG–FTIR–MS detection results is carried out, the main action mechanisms of the two binders are summarized, and a simple schematic diagram is drawn, as shown in Figure 9. During the initial decomposition process, a large number of small molecular substances such as NO2, HONO, H, and OH and large molecular intermediate products such as C4H7O6N7 are generated. Intermediate products will react with each other to form relatively stable products. For example, HONO can react with itself to generate H2O and also can react with C4H7O6N7 to form unstable products, as shown in the Figure S10.39 Moreover, with a hydroxyl group next to the adjacent nitroamine group in C4H7O6N7 molecule will more easily lead to C–N bond breaking and generate small-molecule intermediate products such as CH2O, N2O, and CHN.39,40 The existence of oxidizing active ions (O, HO, etc.) makes the interaction between intermediates easier, but there is a competition mechanism between relatively inert intermediates and oxidizing intermediates, as shown in Figure 9. In the thermal decomposition of the composite particles, the addition of binder BR and F can induce HMX to undergo N–N fracture and H, O dissociation reaction and promote the reaction of small-molecular intermediate products with active ions more quickly. However, the promotion of small-molecule reaction (step 1) by the binder will consume more active ions, which indirectly inhibits the further reaction of relatively inert substances such as C4H7O6N7 (step 2). Moreover, the reaction between binder and HMX intermediate products in the thermal decomposition process will also consume oxidizing active ions. Especially BR, the strong induced adsorption of O seriously affected the thermal decomposition behavior of HMX. This competition mechanism for active ions explains why the decomposition temperature of composite particles is lower, but the activation energy is higher, and the decomposition duration is longer.

Figure 9.

Figure 9

Brief explanation of the action mechanism of the binder in HMX thermal decomposition.

4. Conclusions

DSC–TG–FTIR–MS coupling technology is used to study the mechanism of two different types of binders (BR and F2604) on the thermal decomposition behavior of HMX crystals. It is found that both binders can reduce the decomposition temperature of HMX, induce the decomposition of HMX, and promote the appearance of gas products earlier, while the composite particles have higher activation energy and longer duration of gas product generation. Based on the coupling analysis of DSC–TG–FTIR–GCMS detection results, the mechanism of action of BR and F2604 is proposed, that is, the two binders induce the decomposition of HMX in advance and promote the transformation of small-molecular intermediate fragments into gas products. However, in the oxidation reaction, the existence of the binder makes the small-molecule intermediate fragment more competitive than the inert macromolecular intermediate product, which can consume the active ions in the decomposition process faster, and the reaction of the binder rubber chain also consumes some active ions. Compared with pure HMX crystals, the excessive consumption of active ions in composite particles inhibits the further reaction of inert macromolecular intermediate products such as C4H7O6N7, thereby prolonging the continuous generation time of gas products and slowing down the thermal decomposition process of HMX.

Acknowledgments

The authors wish to thank Miss Li-ping Chen, Lu Liu, and Dr. Ya-jie Chen et al. for their valuable advice and assistant in carrying out the experimental work.

Supporting Information Available

The Supporting Information is available free of charge at https://pubs.acs.org/doi/10.1021/acsomega.0c04985.

  • Morphology of the samples, FTIR test chart of samples at room temperature, thermal analysis test of the binder, reaction process of samples, DSC–TG results of the samples, FTIR diagram of composite particles during thermal decomposition, part GC–MS test results, and possible chemical reactions between intermediates (PDF)

Author Contributions

All authors discussed the results and commented on the manuscript.

This research was supported by the Natural Science Foundation of China (11702142) and the Natural Science Foundation of Jiangsu Province (BK20170825).

The authors declare no competing financial interest.

Supplementary Material

ao0c04985_si_001.pdf (1.3MB, pdf)

References

  1. Dienes J. K.A Unified Theory of Flow, Hot Spots, and Fragmentation with an Application to Explosive Sensitivity. High-Pressure Shock Compression of Solids II; Academic Press: Springer: New York, 1996; pp 366–398. [Google Scholar]
  2. Brousseau P.; Brochu S.; Brassard M.; Ampleman G.; Thiboutot S.; Cote F.; Lussier L. S.; Diaz E.; Tanguay V.; Poulin I.; Beauchemin M... Revolutionary insensitive, green and healthier training technology with reduced adverse contamination project. Proceedings of 40th International Annual Conference of ICT, 1968; Vol. 97; pp 1–9.
  3. Oyumi Y.; Kimura E.; Hayakama S.; Nakashita G.; Kato K. Insensitive munitions ( IM) and combustion characteristics of GAP/AN composite propellants. Propellants, Explos., Pyrotech. 1968, 21, 271–275. [Google Scholar]
  4. Cooper P. W.Explosives Engineering; Academic Press: John Wiley & Sons Inc, 1996; pp 9–36. [Google Scholar]
  5. Norris R. S.; Kristensen H. M.; Handler J. The B61 family of bombs. Bull. At. Sci. 2003, 59, 74–76. 10.2968/059001020. [DOI] [Google Scholar]
  6. Clements B. E.; Mas E. M. A theory for plastic-bonded materials with a bimodal size distribution of filler particles. Modell. Simul. Mater. Sci. Eng. 2004, 12, 407–421. 10.1088/0965-0393/12/3/004. [DOI] [Google Scholar]
  7. Nouguez B.; Mahé B.; Vignaud P. O. Cast PBX related technologies for IM shells and warheads. Sci. Technol. Energetic Mater. 2009, 70, 135–139. [Google Scholar]
  8. Vadhe P. P.; Pawar R. B.; Sinha R. K.; Asthana S. N.; Subhananda Rao A. Cast aluminized explosives. Combust. Explos. Shock Waves 2008, 44, 461–477. 10.1007/s10573-008-0073-2. [DOI] [Google Scholar]
  9. Elbeih A.; Pachman J.; Zeman S.; Trzcínski W. A.; Aǩstein Z.. Advanced plastic explosive based on BCHMX compared with Composition C4 and Semtex 10. Seminar on New Trends in Research of Energetic Materials 14th, 2011; pp 119–126.
  10. Chen J.; Wang J.; Bai C.; Huang H. Preparation and characterization of ε-HNIW booster explosive. Chin. J. Explos. Propellants 2010, 33, 56–59. [Google Scholar]
  11. Borman S. Advanced Energetic Materials Emerge For Military and Space Applications. Chem. Eng. News 2010, 72, 18–22. 10.1021/cen-v072n003.p018. [DOI] [Google Scholar]
  12. Liu J.; Hao G.; Rong Y.; Xiao L.; Jiang W.; Li F.; Jing C.; Gao H.; Chen T.; Ke X. Application and properties of nanometric HMX in PBX. Combust., Explos. Shock 2017, 53, 744–749. 10.1134/s001050821706017x. [DOI] [Google Scholar]
  13. Singh A.; Singh S.; Sharma T. C.; Kishore P. Physicochemical properties and kinetic analysis for some fluoropolymers by differential scanning calorimetry. Polym. Bull. 2018, 75, 2315–2338. 10.1007/s00289-017-2153-5. [DOI] [Google Scholar]
  14. Wang J. Y.; Ye B. Y.; An C. W.; Wu B. D.; Li H. Q.; Wei Y. J. Preparation and Properties of Surface-Coated HMX with Viton and Graphene Oxide. J. Energ. Mater. 2016, 34, 234–245. 10.1080/07370652.2015.1053016. [DOI] [Google Scholar]
  15. Singh A.; Kumar R.; Soni P. K.; Singh V. Compatibility and thermal decomposition kinetics between HMX and some polyester-based polyurethanes. J. Therm. Anal. Calorim. 2020, 10.1007/s10973-020-09377-5. [DOI] [Google Scholar]
  16. Varney A. M.; Strahle W. C. Experimental combustion studies of two-dimensional ammonium perchlorate-binder sandwiches. Combust. Sci. Technol. 1972, 4, 197–208. [Google Scholar]
  17. Fong C. W.; Hamshere B. L. The mechanism of burning rate catalysis in composite HTPB-AP propellant combustion. Combust. Flame 1986, 65, 61–69. 10.1016/0010-2180(86)90073-8. [DOI] [Google Scholar]
  18. Chen J. K.; Brill T. B. Chemistry and kinetics of hydroxyl-termi-nated polybutadiene (HTPB) and diisocyanate-HTPB polymers during slow decomposition and combustion-like conditions. Combust. Flame 1991, 87, 217–232. 10.1016/0010-2180(91)90109-o. [DOI] [Google Scholar]
  19. Kumar R.; Singh A.; Kumar M.; Soni P. K.; Singh V. Investigations of effect of hydroxyl-terminated polybutadiene-based polyurethane binders containing various curatives on thermal decomposition behaviour and kinetics of energetic composites. J. Therm. Anal. Calorim. 2020, 10.1007/s10973-020-09773-x. [DOI] [Google Scholar]
  20. Zeman S.; Elbeih A.; Yan Q.-L. Note on the use of the vacuum stability test in the study of initiation reactivity of attractive cyclic nitramines in Formex P1 matrix. J. Therm. Anal. Calorim. 2013, 111, 1503–1506. 10.1007/s10973-012-2487-z. [DOI] [Google Scholar]
  21. Wei C.-Y.; Lin W.-C.; Pan X.-H.; Shu C.-M.; Hua M.; Jiang H.-C.; Jiang J.-C. Thermal risk assessment of tert-butylperoxy-2-ethylhexyl carbon-ate for storage and transport. J. Therm. Anal. Calorim. 2019, 138, 2891–2900. 10.1007/s10973-019-08552-7. [DOI] [Google Scholar]
  22. Lu Y.-M.; Liu S.-H.; Shu C.-M. Evaluation of thermal hazards based on thermokinetic parameters of 2-(1-cyano-1-methylethyl) azocarboxamide by ARC and DSC. J. Therm. Anal. Calorim. 2019, 138, 2873–2881. 10.1007/s10973-019-08827-z. [DOI] [Google Scholar]
  23. Hussein A. K.; Zeman S.; Elbeih A. Thermo-analytical study of glycidyl azide polymer and its effect on different cyclic nitramines. Thermochim. Acta 2018, 660, 110–123. 10.1016/j.tca.2018.01.003. [DOI] [Google Scholar]
  24. Yan Q.-L.; Zeman S.; Sánchez Jiménez P. E.; Zhao F.-Q.; Pérez-Maqueda L. A.; Málek J. The effect of polymer matrices on the thermal hazard properties of RDX-based PBXs by using model-free and combined kinetic analysis. J. Hazard. Mater. 2014, 271, 185–195. 10.1016/j.jhazmat.2014.02.019. [DOI] [PubMed] [Google Scholar]
  25. Lin C.-P.; Chang Y.-M.; Tseng J.-M.; Shu C.-M. Comparisons of nth-order kinetic algorithms and kinetic model simulation on HMX by DSC tests. J. Therm. Anal. Calorim. 2010, 100, 607–614. 10.1007/s10973-009-0592-4. [DOI] [Google Scholar]
  26. Singh G.; Prem Felix S.; Soni P. Studies on energetic compounds part 28: thermolysis of HMX and its plastic bonded explosives containing Estane. Thermochim. Acta 2003, 399, 153–165. 10.1016/s0040-6031(02)00460-4. [DOI] [Google Scholar]
  27. Singh A.; Sharma T. C.; Kumar M.; Narang J. K.; Kishore P.; Srivastava A. Thermal decomposition and kinetics of plastic bonded explosives based on mixture of HMX and TATB with polymer matrices. Def. Technol. 2017, 13, 22–32. 10.1016/j.dt.2016.11.005. [DOI] [Google Scholar]
  28. Yan Q.-L.; Zeman S.; Zhang X.-H.; Málek J.; Xie W.-X. The mechanisms for desensitization effect of synthetic polymers on BCHMX: physical models and decomposition pathways. J. Hazard. Mater. 2015, 294, 145–157. 10.1016/j.jhazmat.2015.03.063. [DOI] [PubMed] [Google Scholar]
  29. Elbeih A.; Abd-Elghany M.; Elshenawy T. Application of vacuum stability test to determine thermal decomposition kinetics of nitramines bonded by polyurethane matrix. Acta Astronaut. 2017, 132, 124–130. 10.1016/j.actaastro.2016.12.024. [DOI] [Google Scholar]
  30. Yan Q.-L.; Zeman S.; Elbeih A. Thermal behavior and decomposition kinetics of Viton A bonded explosives containing attractive cyclic nitramines. Thermochim. Acta 2013, 562, 56–64. 10.1016/j.tca.2013.03.041. [DOI] [Google Scholar]
  31. Craig M.; Tarver J.; Koerner G. Effects of endothermic binders on times to explosion of HMX- and TATB-based plastic bonded explosives. J. Energ. Mater. 2007, 26, 1–28. 10.1080/07370650701719170. [DOI] [Google Scholar]
  32. Yu Y.; Chen S.; Li X.; Jin S.; Li L.; Zhang G.; Ma X.; Shu Q. The novel compound dimethylamine-5,5-bistetrazole-1,1-diolate: crystal structure, thermal investigation, safety evaluation and theoretical studies. RSC Adv. 2017, 7, 18523–18528. 10.1039/c7ra00908a. [DOI] [Google Scholar]
  33. Wang J.; Chen S.; Yao Q.; Jin S.; Zhao S.; Yu Z.; Li J.; Shu Q. Preparation, Characterization, Thermal Evaluation and Sensitivities of TKX-50/GO Composite. Propellants, Explos., Pyrotech. 2017, 42, 1104–1110. 10.1002/prep.201700080. [DOI] [Google Scholar]
  34. Zou H.-M.; Chen S.-S.; Li X.; Jin S.-H.; Niu H.; Wang F.; Chao H.; Fang T.; Shu Q.-H. Preparation, thermal investigation and detonation properties of ε-CL-20-based polymer-bonded explosives with high energy and reduced sensitivity. Mater. Express. 2017, 7, 199–208. 10.1166/mex.2017.1366. [DOI] [Google Scholar]
  35. Wu Z.; Pei J.; Song X.; Liu N.; Li J.; Zhang M.; Zhang J.; Zhang D.; Zhao F. The catalytic effects of nano-Fe2O3 and Rgo-Fe2O3 on the thermal decomposition properties of CL-20/HMX cocrystals. New J. Chem. 2020, 44, 1858–1864. 10.1039/c9nj05619j. [DOI] [Google Scholar]
  36. Patidar L.; Khichar M.; Thynell S. T. A comprehensive mechanism for liquid-phase decomposition of 1,3,5,7-tetranitro-1,3,5,7-tetrazoctane (HMX): Thermolysis experiments and detailed kinetic modeling. Combust. Flame 2020, 212, 67–78. 10.1016/j.combustflame.2019.10.025. [DOI] [Google Scholar]
  37. Brill T. B.; Gongwer P. E.; Williams G. K. Thermal Decomposition of Energetic Materials. 66. Kinetic Compensation Effects in HMX, RDX, and NTO. J. Phys. Chem. A 1994, 98, 12242–12247. 10.1021/j100098a020. [DOI] [Google Scholar]
  38. Tarver C. M.; Chidester S. K.; Nichols A. L. Critical Conditions for Impact- and Shock-Induced Hot Spots in Solid Explosives. J. Phys. Chem. B 1996, 100, 5794–5799. 10.1021/jp953123s. [DOI] [Google Scholar]
  39. Patidar L.; Khichar M.; Thynell S. T. Identification of initial decomposition reactions in liquid-phase hmx using quantum mechanics calculations. Combust. Flame 2018, 188, 170–179. 10.1016/j.combustflame.2017.09.042. [DOI] [Google Scholar]
  40. Melius C. F.; Piqueras M. C. Initial reaction steps in the condensed-phase decomposition of propellants. Proc. Combust. Inst. 2002, 29, 2863–2871. 10.1016/s1540-7489(02)80350-9. [DOI] [Google Scholar]
  41. Málek J. Crystallization kinetics by thermal analysis. J. Therm. Anal. 1999, 56, 763–769. 10.1023/a:1010106206509. [DOI] [Google Scholar]
  42. Málek J. The kinetic analysis of non-isothermal data. Thermochim. Acta 1992, 200, 257–269. 10.1016/0040-6031(92)85118-f. [DOI] [Google Scholar]
  43. Málek J. Kinetic analysis of crystallization processes in amorphous materials. Thermochim. Acta 2000, 355, 239–253. 10.1016/s0040-6031(00)00449-4. [DOI] [Google Scholar]

Associated Data

This section collects any data citations, data availability statements, or supplementary materials included in this article.

Supplementary Materials

ao0c04985_si_001.pdf (1.3MB, pdf)

Articles from ACS Omega are provided here courtesy of American Chemical Society

RESOURCES