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Maximising the heritage of the existing ISIS ISIPOD cubesat deployers family, and building on past studies performed within ESA GSP such as LV-POD, (Low-Velocity deployer),the main task of this TFO activity will be to :-Design a Low-Velocity 6U deployer suitable for deep space missions, compatible with the low separation velocity (order cm/s) and rotation error needed for deep space mission such as Hera, taking into account a series of requirements injected by the agency -Define interfaces w.r.t.

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The increasing interest for Deep-Space cubesat is leading in the near future to the need of adequate deployment systems (``Cubesat Dispensers``) suitable for deep space applications, taking into account all the environmental (e.g. radiation) and mission constraints (e.g. need for power supply to the cubesat, possibility to upload SW updates, need for accurate release conditions).

The activity is aiming at developing a new generation of mass memories able to support File Based Operations while sustaining high data throughput and providing large capacity.

The project called Peripheral and Redundancy Switch Controller is based on the proposal made by Agile Systems Engineering to develop, test and integrate a switch between two on-board-computers (OBCs) that would be connected to

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