Laura Miquel Parra , Telespazio Belgium for ESA/ESTEC
CubeSat missions are growing in the space sector, facing the challenges related to the implementation of space debris mitigation requirements as any other mission would. In the RAMS domain, it is becoming necessary to adapt the level of expected reliability assessment to the needs of the spacecrafts and their missions, depending on aspects such as the existence of a satellite reliability requirement or whether the constellation the spacecraft is part of has some constellation/system/service availability requirement.
The proposed presentation explains the steps of reliability modelling to be followed to state compliance to the applicable probabilistic disposal requirements for CubeSats.