Analysis of the radiation sector on a nanosatellite, using a Radiation Model based on a 1U CubeSat or a 3U CubeSat standard [CDS] which includes at least: deployable solar panel(s), deployable antenna(s), magneto-torquer(s), reaction wheel(s), a battery set, 3 solar sensor(s), an Aluminum structure and various PCB with EEE parts.

University of Montpellier (France)