- Conference Article
- 10.2514/6.2026-2880
Analytical Mechanics of Ceramics and Fiber-Reinforced CMCs for Material Processing Foundations of Rocket Nozzles: Stage I
- Jan 08, 2026
- Nestor Cano + 6 more +6
This work presents Stage I of a multi-phase research effort focused on the analytical and computational development of ceramic-matrix composite (CMC) rocket nozzle components, with consideration given to feasible manufacturing approaches for future prototype fabrication. High-purity Alumina 4N, Calcined Alumina, and Nextel™ 720 or 610 fibers were evaluated as candidate materials for high-temperature propulsion environments, with additive manufacturing and powder-sintered composite processing identified as viable fabrication pathways for subsequent project phases. A combined analytical framework incorporating micromechanics-based lamina modeling, Classical Laminate Theory, and spatially varying pressure and thermal loading derived from quasi-one-dimensional compressible-flow analysis was developed to predict laminate stresses and strain margins along the nozzle contour. Ply-level composite behavior was evaluated using ANSYS ACP structural simulations, while a steady-state thermal model employing a homogenized orthotropic composite representation was used to resolve temperature gradients and thermally induced deformation. Together, these numerical analyses define critical loading regions, quantify structural safety margins, and establish preliminary material selection, geometry, and thermo-mechanical design requirements that will guide future laminate fabrication efforts and experimental hot-fire testing of CMC nozzle prototypes.
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