Copyright (c) 2026 SSNM SANTOSH MADA, VAIBHAV S. SADAVARTE, RAMESH KURVA, SHRIKANT M. PANDE, PRASHANT S. KULKARNI

This work is licensed under a Creative Commons Attribution 4.0 International License.
Effect of 1,1-Diamino-2,2-Dinitroethene (FOX-7) on Thermal Decomposition of Cyclotetramethylenetetranitramine (HMX) and Combustion of Reduced Smoke Propellants
Corresponding Author(s) : S.S.N.M. Santosh Mada
Asian Journal of Chemistry,
Vol. 38 No. 6 (2026): Vol. 38 Issue No 6, 2026
Abstract
The development of next generation solid rocket propellant requires a critical balance between high energy output and insensitivity to mechanical stimuli. This study investigates the thermal decomposition of cyclotetramethylenetetranitramine (HMX) in combination with 1,1-diamino-2,2-dinitroethene (FOX-7) and other propellant ingredients. Mixture of FOX-7 and HMX was analysed by SEM and XRD techniques to understand the type of interactions formed during sample preparation by wet grinding process. Further, thermogravimetric analysis coupled with FTIR (TG-FTIR) was employed to investigate the thermal decomposition behaviour of HMX/FOX-7 binary mixtures and solid propellant formulations containing butanetriol trinitrate, polycaprolactone polyol prepolymer, HMX, FOX-7 and ammonium perchlorate (AP). In this study, neat HMX exhibited a single sharp exothermic peak at 285.7 ºC, whereas FOX-7 decomposed in two stages at 230.5 and 293.9 ºC. Decompositions occurred at 225.2 ºC, 254.1 ºC and 285.0 ºC in 1:1 HMX/FOX-7 mixture, indicating significant mutual interaction between the two components. Similar type of interaction was also observed in thermal decomposition of FOX-7/AP combination. In addition, a systematic study of binary mixtures was conducted to understand the mutual effect of FOX-7 on thermal decomposition of HMX. An attempt to predict the mechanism of mutual effect of FOX-7 and HMX on thermal decomposition of 1:1 mixture has also been made by FTIR absorbance intensity of gases evolved at maximum heat release. Propellants designated as P-1, P-2 and P-3 were formulated using unary, binary and ternary solid mixtures of FOX-7, HMX and AP, respectively, and were characterized for density, sensitivity and thermal stability. It was observed that pressure dependencies of P-2 and P-3 were reduced by ~6% and ~11%, respectively as a result of the mutual effect among the propellant ingredients.
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- Z.-H. Xue, Z.-K. Wang, R.-X. Xu, X.-X. Zhang and Q.-L. Yan, Energ. Mater. Front., 3, 209 (2022); https://doi.org/10.1016/j.enmf.2022.01.005
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- K. Menke and S. Eisele, Propellants Explos. Pyrotech., 22, 112 (1997); https://doi.org/10.1002/prep.19970220304
- C. Oommen and S.R. Jain, J. Hazard. Mater., 67, 253 (1999); https://doi.org/10.1016/S0304-3894(99)00039-4
- I. Powell, Reduced Vulnerability Minimum Smoke Propellants For Tactical Rocket Motors, Proceedings of 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference, AIAA Paper 2005-3615 (2005); https://doi.org/10.2514/6.2005-3615
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- V.P. Sinditskii, A.I. Levshenkov, V.Y. Egorshev and V.V. Serushkin, Proceeedings of 30th International Pyrotechnic Seminar, France, p. 299 (2003).
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- M. Ghosh, A.K. Sikder, S. Banerjee, M.B. Talawar and N. Sikder, Def. Technol., 16, 188 (2020); https://doi.org/10.1016/j.dt.2019.05.018
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- J. Welch, Ph.D. Thesis, Low Sensitivity Energetic Materials Ludwig Maximilian University of Munich (2008).
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- T.B. Brill, J. Propuls. Power, 11, 740 (1995); https://doi.org/10.2514/3.23899
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References
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J. Dong, J. Peng, C. Li, J. Ou, and J. Liu, Cent. Eur. J. Energ. Mater., 22, 344 (2025); https://doi.org/10.22211/cejem/211476
A.N. Pivkina, N.V. Muravyev, K.A. Monogarov, V.G. Ostrovsky, I.V. Fomenkov, Y.M. Milyokhin and N.I. Shishov, in eds.: L. De Luca, T. Shimada, V. Sinditskii and M. Calabro, Synergistic Effect of Ammonium Perchlorate on HMX: From Thermal Analysis to Combustion, In: Chemical Rocket Propulsion, Springer, pp 365-381 (2017); https://doi.org/10.1007/978-3-319-27748-6_15
K. Hwang, H. Mun, J.Y. Jung, H.L. Cho, S.J. Kim, B.S. Min, H.B. Jeon and W. Kim, Polymers, 11, 1966 (2019); https://doi.org/10.3390/polym11121966
S.M. Pande, V.S. Sadavarte, D. Bhowmik, D.D. Gaikwad, R.V. Singh and H. Singh, Propellants Explos. Pyrotech., 37, 241 (2012); https://doi.org/10.1002/prep.201000149
K. Menke and S. Eisele, Propellants Explos. Pyrotech., 22, 112 (1997); https://doi.org/10.1002/prep.19970220304
C. Oommen and S.R. Jain, J. Hazard. Mater., 67, 253 (1999); https://doi.org/10.1016/S0304-3894(99)00039-4
I. Powell, Reduced Vulnerability Minimum Smoke Propellants For Tactical Rocket Motors, Proceedings of 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference, AIAA Paper 2005-3615 (2005); https://doi.org/10.2514/6.2005-3615
M. Nagamachi, J. Oliveira, A. Kawamoto and R. Dutra, J. Aerosp. Technol. Manag., 1, 153 (2009); https://doi.org/10.5028/jatm.2009.0102153160
K. Menke, T. Heintz, W. Schweikert, T. Keicher and H. Krause, Propellants Explos. Pyrotech., 34, 218 (2009); https://doi.org/10.1002/prep.200900013
N. Wingborg, S. Andreasson, J. de Flon, M. Johnsson, M. Liljedahl, C. Oscarsson, Å. Pettersson and M. Wanhatalo, Development of ADN-Based Minimum Smoke Propellants, Proceeding of 46th AIAA/ASME/ SAE/ASEE Joint Propulsion Conference, AIAA Paper 2010-6586 (2010); https://doi.org/10.2514/6.2010-6586
C. Grigore and D.M. Alexandru, INCAS Bull., 9, 17 (2017); https://doi.org/10.13111/2066-8201.2017.9.1.2
I.J. Lochert, DSTO-TR-1238, Defence Science and Technology Organisation (2001).
V.P. Sinditskii, A.I. Levshenkov, V.Y. Egorshev and V.V. Serushkin, Proceeedings of 30th International Pyrotechnic Seminar, France, p. 299 (2003).
A.K. Burnham, R.K. Weese, R. Wang, Q.S.M. Kwok and D.E.G. Jones, Thermal Properties of FOX-7, Proceedings of 36th International Annual Conference of ICT & 32nd International Pyrotechnics Seminar, Karlsruhe, Germany, 28 June-1 July (2005).
R.S. Booth and L.J. Butler, J. Chem. Phys., 141, 134315 (2014); https://doi.org/10.1063/1.4896165
W.A. Trzciński and A. Belaada, Cent. Eur. J. Energ. Mater., 13, 527 (2016); https://doi.org/10.22211/cejem/65000
M. Ghosh, A.K. Sikder, S. Banerjee, M.B. Talawar and N. Sikder, Def. Technol., 16, 188 (2020); https://doi.org/10.1016/j.dt.2019.05.018
P.B. Kempa, M. Hermann, F.J.M. Metzger, V. Thome, A. Kjellstroem and N. Latypov, Proceedings of 35th International Annual Conference ICT, pp. 71/1-71/5 (2004).
R. Wild and U. Teipel, Proceedings of 35th International Annual Conference ICT, p. 69/1-69/9 (2004).
J. Welch, Ph.D. Thesis, Low Sensitivity Energetic Materials Ludwig Maximilian University of Munich (2008).
M.J. Crawford, J. Evers, M. Göbel, T.M. Klapötke, G. Oehlinger, P. Mayer and J.M. Welch, Propellants Explos. Pyrotech., 32, 478 (2007); https://doi.org/10.1002/prep.200700240
D.S. Viswanath, T.K. Ghosh and V.M. Boddu, FOX-7 (1,1-Diamino-2,2-Dinitroethylene), In: Emerging Energetic Materials: Synthesis, Physicochemical and Detonation Properties. Springer (2018); https://doi.org/10.1007/978-94-024-1201-7_3
O. Ordzhonikidze, A. Pivkina, Y. Frolov, N. Muravyev and K. Monogarov, J. Therm. Anal. Calorim., 105, 529 (2011); https://doi.org/10.1007/s10973-011-1562-1
S. Vyazovkin, Molecules, 25, 2813 (2020); https://doi.org/10.3390/molecules25122813
A. Kumar, V.S. Sadavarte, S.S.N.M. Santosh Mada, S.M. Pande and P.V. Chavan, Propellants Explos. Pyrotech., 46, 626 (2021); https://doi.org/10.1002/prep.202000241
N. Koga, S. Vyazovkin, A.K. Burnham, L. Favergeon, N.V. Muravyev, L.A. Perez-Maqueda, C. Saggese and P.E. Sanchez-Jiménez, Thermochim. Acta, 719, 179384 (2023); https://doi.org/10.1016/j.tca.2022.179384
J. Yu, H. Jiang, S. Xu, H. Li, Y. Wang, E. Yao, Q. Pei, M. Li, Y. Zhang and F. Zhao, Crystals, 13, 167 (2023); https://doi.org/10.3390/cryst13020167
X.Y. Liu, X.C. Wang, Y.G. Huang, M.X. Zheng, L. Wang, Y. Jiang and Y.W. Luo, Guangpuxue Yu Guangpu Fenxi, 26, 251 (2006).
Y. Xu, R. Chen, Y. Liu, Y. Wang and W. Zheng, J. Anal. Appl. Pyrol., 195, 107701 (2026); https://doi.org/10.1016/j.jaap.2026.107701
T.B. Brill, J. Propuls. Power, 11, 740 (1995); https://doi.org/10.2514/3.23899
Z. Fengqi, G. Hongxu, X. Siyu, Y. Jianhua, P. Qing, H. Haixia and X. Xiaoling, Chin. J. Explos. Propellants, 33(4), 1 (2010) (In Chinese).
C. Zhong’e, L. Zhongyou, Y. Nan, L. Qing and W. Du, Chin. J. Energ. Mater., 18, 316 (2010) (In Chinese); https://doi.org/10.3969/j.issn.1006-9941.2010.03.017
D.B. Lempert, E.M. Dorofeenko and Y. Shu, Russ. J. Phys. Chem. B. Focus Phys., 10, 483 (2016); https://doi.org/10.1134/S1990793116030258
T.L. Jensen, E. Unneberg and T.E. Kristensen, Propellants Explos. Pyrotech., 42, 381 (2017); https://doi.org/10.1002/prep.201600278
W. Xie, Y. Zhao, W. Zhang, Y. Liu, X. Fan, B. Wang, W. He and Q.-L. Yan, Propellants Explos. Pyrotech., 43, 308 (2018); https://doi.org/10.1002/prep.201700251
M.W. Beckstead, Combust. Explos. Shock Waves, 42, 641 (2006); https://doi.org/10.1007/s10573-006-0096-5
S. Isert and S.F. Son, in eds.: M. Shukla, V. Boddu, J. Steevens, R. Damavarapu and J. Leszczynski, Energetic Materials, Springer, vol. 25 (2017); https://doi.org/10.1007/978-3-319-59208-4_6