Ablative thermal protection systems. The project will study ablative reentry heat shields by experiments simulating hypervelocity atmospheric flight. The results will enable the design of the advanced spacecraft which are needed to extend mans exploration of the universe. Data will be validated by comparison with flights such as the Japanese Hayabusa asteroid sample return mission.
Designing Radiation-Tolerant Reconfigurable Systems for Space. The processing speed, cost and flexibility requirements of future satellite-based applications cannot be satisfied with conventional radiation-hardened processors or custom integrated circuits. This project aims to develop key technology to enable off-the-shelf hardware to be customised for this use without compromising reliability. The project aims to develop the design methods needed to implement a given set of satellite applicatio ....Designing Radiation-Tolerant Reconfigurable Systems for Space. The processing speed, cost and flexibility requirements of future satellite-based applications cannot be satisfied with conventional radiation-hardened processors or custom integrated circuits. This project aims to develop key technology to enable off-the-shelf hardware to be customised for this use without compromising reliability. The project aims to develop the design methods needed to implement a given set of satellite applications on a processing platform composed of application-specific soft processors and accelerator circuits hosted on conventional reconfigurable logic devices. Crucially, the solution architecture is expected to be sufficiently hardened against radiation-induced errors while meeting performance and circuit area constraints.Read moreRead less