Design of the radiation shielding for a microsatellite

This paper aims to provide a detailed description of the problems concerning the radiation environment faced while designing a microsatellite at the University of Rome. Although main features of the microsatellite, as well as the environment characteristics expected in candidate orbits are detailed, emphasis is given to expose a generally appropriate procedure for this class of spacecraft. The sector analysis is carried on. and a simple qualitative way to point out critical areas of shielding is shown. The risk concerning the specific devices is assessed, both for total ionization dose and single event upset. The effect of the spot shielding on the most sensitive devices is considered, in order to mitigate SEE occurrence. (C) 2002 International Astronautical Federation. Published by Elsevier Science Ltd. All rights reserved.