Building a mathematical model describing the dome profile of a solid fuel engine case made from composite materials using winding technology

8 views

Authors

  • Tran Ngoc Thanh Institute of Missile, Academy of Military Science and Technology
  • Dinh Van Hien Institute of Missile, Academy of Military Science and Technology
  • Bui Van Am (Corresponding Author) Institute of Missile, Academy of Military Science and Technology

DOI:

https://doi.org/10.54939/1859-1043.j.mst.109.2026.146-153

Keywords:

Solid fuel engine case made from composite material; Dome profile; Axial force; Nozzle radius.

Abstract

With the advantage of high specific strength, composite materials are the first choice for manufacturing a solid fuel engine case to increase the engine's stuffing coefficient. The main problem for designing an engine case from composite materials is the problem of determining the dome profile of the engine case. To determine the dome profile based on continuum theory, the article focuses on building a general mathematical model describing the dome profile of the case with an internal thermal protection layer under internal pressure p and axial force. Using this mathematical model, the influence of axial force and nozzle radius on the dome profile of the engine case is analyzed. The results of the article are the basis for designing the case of a solid fuel engine from composite materials.

References

[1]. Agarwal, B. D.; Broutman, L. J.; Chandrashekhara, K., “Analysis and Performance of Fiber Composites”, Wiley, New Jersey, (2006).

[2]. Liang, C. C.; et al., “Optimum design of dome contour for filament-wound composite pressure vessels based on a shape factor”, Composite Structures, Vol. 58, No. 4, pp. 469–482, (2002). DOI: https://doi.org/10.1016/S0263-8223(02)00136-8

[3]. Hien, D. V.; Thanh, T. N.; et al., “Design of planar wound composite vessel based on preventing slippage tendency of fibers”, Composite Structures, Vol. 254, Article 112820, (2020). DOI: https://doi.org/10.1016/j.compstruct.2020.112854

[4]. Milligan, D. J.; Ghoshal, A., “Design and Analysis of a Composite-Lined Rocket Motor Case”, NASA Technical Memorandum 107523, NASA Langley Research Center, Hampton, VA, (1992).

[5]. Wen, J.; Wu, Y., “Effect of high temperature on mechanical properties and porosity of carbon fiber/epoxy composites”, Composite Structures, Vol. 262, Article 113640, (2021).

[6]. Zu, L.; et al., “Design of filament-wound domes based on continuum theory and non-geodesic roving trajectories”, Composites Part A, Vol. 41, pp. 1312–1320, (2010). DOI: https://doi.org/10.1016/j.compositesa.2010.05.015

[7]. U.S. Department of Defense, “MIL-HDBK-17-1F: Composite Materials Handbook, Volume 1 – Polymer Matrix Composites Guidelines for Characterization of Structural Materials”, Department of Defense, Washington, D.C., (2002).

[8]. Vasiliev, V. V.; Krikanov, A. A., “New generation of filament-wound composite pressure vessels for commercial applications”, Composite Structures, Vol. 62, No. 3, pp. 449–459, (2003). DOI: https://doi.org/10.1016/j.compstruct.2003.09.019

[9]. Vasiliev, V. V., “Composite Pressure Vessels: Analysis, Design, and Manufacturing”, Bull Ridge Publishing, Blacksburg, Virginia, USA, (2009).

[10]. Калинчев, В. А.; Ягодников, Д. А., “Технология производства ракетных двигателей твердого топлива”, Технологии ракетно-космического машиностроения, Vol. 688, Moscow, (2010).

[11]. Буланов, И. М.; Смыслов, В. И.; Комков, М. А.; Кузнецов, В. И., “Сосуды давления из композиционных материалов в конструкциях летательных аппаратов”, Moscow, (1985).

Downloads

Published

25-02-2026

How to Cite

[1]
Tran Ngoc Thanh, Dinh Van Hien, and V. Ấm Bùi, “Building a mathematical model describing the dome profile of a solid fuel engine case made from composite materials using winding technology”, J. Mil. Sci. Technol., vol. 109, no. 109, pp. 146–153, Feb. 2026.

Issue

Section

Mechanics & Mechanical Engineering

Most read articles by the same author(s)