Hera mission analysis: Milani and Juventas cubesats

The dissertation is about the Hera mission, it is an analysis of the three spacecraft: Hera itself, Milani and Juventas. In the first part, a general presentation of the mission is done: from the payload of the satellite to the orbit around Didymos system. Milani cubesat analysis is the focus of the second part, where deep discussion on the attitude control and the reason behind is presented, as well as an analysis of the SRP effect, orbit and the EOL options. The last section of the dissertation is revolved around Juventas cubesat: its science phase, orbit, payload and EOL options.