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The research aims to design and evaluate a solid-propellant model rocket considering various engineering aspects.

February 2, 2026Open Access

Integrated Aerodynamic and Structural Design with Experimental Evaluation of a Solid-Propellant Model Rocket

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This work demonstrates design and experimental evaluation of a solid-propellant model rocket, indicating its reliable performance.

The research aims to design and evaluate a solid-propellant model rocket considering various engineering aspects.
Integrated propulsion, aerodynamic, structural, and avionics systems into a complete rocket design.
Utilized numerical simulation alongside experimental testing for validation.
Employed finite-element analysis to ensure structural integrity.
Applied computational fluid dynamics for aerodynamic stability in subsonic conditions.
Conducted ground testing with static motor firings and recovery system checks.
Achieved a flight-ready system with satisfactory structural and stability parameters.
Demonstrated effective subsystem operation prior to launch.
Established a design-test feedback loop to minimize model uncertainty.

Nikolaou et al. (2025) studied this question.

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