There is a need within the space sector of medium to high resolutions rotatory position sensors suitable for low cost, space qualified and off-the-shelf solutions. The developed sensor could be used for SADM, optical pointing mechanisms, antennas drive mechanism among others.

We have continued our shock physics code calculation studies of DART-like impact events. This includes comparisons of iSALE and SPH code calculations, using a range of strength and structural properties. The effect of porosity was studied in detail by applying different crushcurves, representing materials with varying crushing strength. The crushcurve was found to have a large influence on the outcome, in particular the ejecta properties and momentum transfer.

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The project aimed to establish a structured approach to an optimised part or component by applying Concurrent Design methods. It intended to incorporate all necessary disciplines and competencies that are required for a potential spacecraft part. Within the activity, advanced manufacturing included various novel techniques, not only additive manufacturing. It means that the Concurrent Design approach was developed for the engineering of units to be built with a broad range of advanced manufacturing technologies.

The main tasks of this activity are the following: 1) Metrological assessment and gap analysis of existing thermal imaging methodology, data processing and uncertainty assessment, related but not limited to aerospace applications.