Aeroelasticity and Dynamics of Deployable Space Structures The University of Manchester in United Kingdom

The PhD project "Aeroelasticity and Dynamics of Deployable Space Structures" at The University of Manchester offers an exciting opportunity to explore the complex interplay between structural flexibility, inertial forces, and environmental interactions in space engineering. Deployable structures such as solar arrays, antennas, habitats, and scientific instruments are essential for space missions, requiring reliable unfolding and operational stability in low-gravity or planetary environments like the Moon and Mars.

These structures utilize lightweight, flexible materials to minimize mass and maximize stowage efficiency, but their deployment introduces significant aeroelastic and structural dynamics phenomena. Even in near-vacuum or low-pressure environments, rapid deployment can induce vibrations, buckling, and coupled deformation modes, impacting stability and longevity. The project aims to develop comprehensive theoretical and computational models to analyze these coupled dynamics, providing predictive insights into deformation, oscillation modes, and deployment performance under dynamic loads, thermal stresses, and environmental factors such as dust and micrometeoroid impacts.

Key objectives include:

• Developing mathematical and computational models for structural deformation, inertial loads, and environmental forces during deployment and operation.
• Quantifying the influence of membrane stiffness, hinge flexibility, mass distribution, and damping on reliability, vibration modes, and functional stability.
• Optimizing structure design for consistent deployment, long-term stability, and resistance to dynamic perturbations in lunar, Martian, or orbital conditions.
• Simulating environmental interactions to guide material and mechanism selection.
• Providing mission planning insights, including optimal deployment sequences, robotic control strategies, and real-time structural health monitoring.

Applicants should have a strong academic background in science or engineering, with at least a 2.1 honours degree or a master’s (or international equivalent). The project is based in the Department of Mechanical and Aerospace Engineering, and excellent candidates will be nominated for competence-based faculty funding, covering tuition fees and a tax-free stipend at the UKRI rate (£20,780 for 2025/26). The stipend is expected to increase annually. Self-funded students are also welcome to apply.

Applications are accepted year-round, but early submission is recommended as the advert may be removed before the deadline. Flexible study arrangements, including part-time options, are available depending on project and funding. The University of Manchester is committed to equality, diversity, and inclusion, actively encouraging applicants from diverse backgrounds and career paths.

To apply, candidates should contact the supervisor to discuss their academic background and motivation, then submit an online application with all required documents, including transcripts, CV, supporting statement, and referee contact details. For further information or questions, contact the admissions team at [email protected].