- Special user interface developed for space applications.
- The three-dimensional geometries can be prepared by user in STEP format for the simulation.
- STEP format is converted to GDML by MRADSIM.
- The orbit parameters of the satellite are created with SPENVIS and the radiation types and quantities are determined.
- Physical processes and limits are specified.
- The simulation is carried out and the results are produced in many formats as graphical analyses.