Influence of trans 1,4,5,8-tetranitrosotetraazadecalin on mechanical integrity and microstructure of composite modified double base propellant

Authors

  • Do Duc Tri Institute of Materials, Biology and Environment/Academy of Military Science and Technology
  • Pham Thanh Dat Institute of Propellant and Explosives
  • Hoang The Vu Institute of Propellant and Explosives
  • Nguyen Manh Tuong (Corresponding Author) Institute of Materials, Biology and Environment/Academy of Military Science and Technology

DOI:

https://doi.org/10.54939/1859-1043.j.mst.IMBE.2025.36-42

Keywords:

Ballistite propellant; Trans-1,4,5,8-tetranitrosotetraazadecalin; Dynamic mechanical analysis (DMA); Composite modified double base propellant; Energetic additives.

Abstract

This study investigates the influence of trans-1,4,5,8-tetranitrosotetraazadecalin (TNSTAD) (20-30% loadings) on the mechanical properties of composite modified double base (CMDB) propellant. A counterintuitive finding emerged: TNSTAD simultaneously enhances both stiffness (storage modulus) and mechanical damping (tan δ). Dynamic Mechanical Analysis (DMA) revealed a 14% increase in the tan δ peak, signaling new energy dissipation, while the rubbery-state modulus nearly doubled. Notably, the α-transition width (FWHMα) narrowed significantly (36.0 °C to ~ 25 °C), suggesting a more homogeneous relaxation spectrum due to uniform stress fields created by well-dispersed particles. Quasi-static tests confirmed significant reinforcement tensile strength increased by 33.7% and Young's modulus doubled, albeit with a 64% reduction in ductility. SEM fractography identified weak interfacial adhesion and debonding as primary failure mechanisms. We propose that interfacial frictional sliding at these weak interfaces is responsible for the enhanced damping. Despite the damping-ductility trade-off, TNSTAD yields a favorable stiffness-damping balance, promising improved stability and vibration tolerance.

References

[1]. Lewczuk, R., and K. Gańczyk-Specjalska, "Modern Highly Energetic Materials for the Production of Gun Powders and Rocket Propellants in Poland," Central European Journal of Energetic Materials, 19(3), (2022).

[2]. Szala, M., "Development trends in artillery ammunition propellants," Materiały Wysokoenergetyczne, 12(2), pp. 5–16, (2020).

[3]. Shoukry, S., M. Ismail, and A. Abd Elgwad, "Performance and stability of modern gun propellants," The International Conference on Chemical and Environmental Engineering, Military Technical College, (2008).

[4]. Jaiswal, G., et al., "RDX based enhanced energy propellant for tank gun ammunition," Propellants, Explosives, Pyrotechnics, 45(3), pp. 472–479, (2020).

[5]. Davenas, A., "Development of modern solid propellants," Journal of Propulsion and Power, 19(6), pp. 1108–1128, (2003).

[6]. Phuong, T. V., "Nghiên cứu tổng hợp chất trans-1, 4, 5, 8 tetranitroso-1,4,5,8 tetraazadecalin (Ц-2) ứng dụng làm phụ gia năng lượng cho thuốc phóng AПЦ-235П của đạn 125 mm trên xe tăng T90S," Journal of Military Science and Technology, (74), pp. 59–63, (2021) (in Vietnamese).

[7]. Prabhakaran, K., N. Bhide, and E. Kurian, "XRD, spectroscopic and thermal analysis studies on trans-1, 4, 5, 8-tetranitiosotetraazadecalin (TNSTAD)," Thermochimica Acta, 220, pp. 169–183, (1993).

[8]. Жуков, Б., "Энергетические конденсированные системы. Краткий энциклопедический словарь," Янус-К, Москва, (1999).

[9]. Bashir, M. A., "Use of dynamic mechanical analysis (DMA) for characterizing interfacial interactions in filled polymers," Solids, 2(1), pp. 108–120, (2021).

[10]. Fu, S.-Y., et al., "Effects of particle size, particle/matrix interface adhesion and particle loading on mechanical properties of particulate–polymer composites," Composites Part B: Engineering, 39(6), pp. 933–961, (2008).

[11]. Pomogailo, A. D., "Hybrid polymer-inorganic nanocomposites," Russian Chemical Reviews, 69(1), pp. 53–80, (2000).

Downloads

Published

18-11-2025

How to Cite

[1]
Do Duc Tri, Pham Thanh Dat, Hoang The Vu, and Nguyen Manh Tuong, “Influence of trans 1,4,5,8-tetranitrosotetraazadecalin on mechanical integrity and microstructure of composite modified double base propellant”, JMST, no. IMBE, pp. 36–42, Nov. 2025.

Issue

Section

Chemistry, Biology & Environment

Most read articles by the same author(s)