“…There are several factors regarding the space environment having the highest impact on dependability and overall availability of the satellite system's space segment. This includes space radiation, high temperature variations, lack of convection, ultrahigh vacuum, etc [1]. It has been simulated (using SPENVIS [2]), that for short-term CubeSat Low-Earth Orbit (LEO) missions, the average Total Ionising Dose (TID) accumulated in silicon specimen, originating from solar proton and electron radiation as well as these coming from other extraterrestrial sources (including trapped particles and high energy ions) should not exceed a level of several krad per each monthly existence on the orbit, if basic shielding is used.…”