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A Numerical Study on Carbon-Fiber-Reinforced Composite Cylindrical Skirts for Solid Propeller Rockets
Ferdinando Baldieri1, Emanuele Martelli1, Aniello Riccio1
1Department of Engineering, University of Campania "L. Vanvitelli", Via Roma 29, 81031 Aversa, Italy.
Researchers compared steel and carbon-fiber composite skirts for solid rocket motors (SRMs). The composite skirt demonstrated superior performance, offering a potential weight reduction for increased flight range.
Area of Science:
- Aerospace Engineering
- Materials Science
- Computational Fluid Dynamics
Background:
- Solid rocket motors (SRMs) are crucial for space propulsion.
- Reducing SRM weight is key to enhancing flight range.
- The combustion chamber skirt is a potential area for weight optimization.
Purpose of the Study:
- To investigate the structural behavior of a cylindrical skirt under internal pressure and axial thrust.
- To compare the performance of a steel skirt with a carbon-fiber-reinforced composite skirt.
- To assess the viability of composite materials for SRM skirt applications.
Main Methods:
- Simulating the flowfield using an axisymmetric k-ω turbulence model.
- Modeling the carbon-fiber-reinforced composite skirt with a [90/0/45/-45]s layup using classical laminate theory.
- Applying Hashin's failure criteria for composite layer integrity and linearized buckling methods for buckling analysis.
Main Results:
- The study analyzed the structural response and buckling behavior of both steel and composite skirts.
- The composite skirt's performance was evaluated against a standard steel skirt under operational loads.
- Key performance metrics related to structural integrity and weight were compared.
Conclusions:
- Carbon-fiber-reinforced composite skirts present a viable alternative to traditional steel skirts.
- The use of composite materials can lead to significant weight reduction in solid rocket motors.
- This weight optimization has the potential to increase the overall flight range of SRM-powered vehicles.
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