Total ionizing dose (TID) and displacement damage (DD) analyses for different space missions.

There are three fundamental effects of space radiation that need considering for successful space missions, namely Total Ionizing Dose, Displacement Damage, and Single Event Effects. While Single Event Effect emerges from transient phenomena, Total Ionizing Dose and Displacement Damage are cumulative effects that threaten the performance of satellite electronics. In this study, we tried to present the results of these effects for different space mission parameters. The conceptual satellites with different shielding (structural material) thicknesses were generated for this purpose. We chose the Aluminum (Al) as shielding material with different thicknesses, such as 0.5, 1, 2, 3, 4, and 5 mm. Subsequently, we performed the analyses with these structural models for different orbit parameters (space missions), i.e., Low Earth Orbit (LEO), Medium Earth Orbit (MEO), Geostationary Orbit (GEO), and Highly Elliptical Orbit (HEO). [ABSTRACT FROM AUTHOR]