MAC Attitude Control (IDR/UPM)
This experiment is part of an internal IDR/UPM program to develop robust attitude control schemes based on the magnetic field, to be applied in future flights, and which will be tested in this flight as experiments.
CTM Thermal Control (IDR/UPM)
This experiment is part of an internal IDR/UPM programme. It aims to obtain data on the satellite’s operation and its thermal behaviour, in order to refine the thermal design and calculation methods in which IDR/UPM has extensive experience.
RW Reaction Wheel (SSBV)
SSBV provides the satellite with a miniature reaction wheel, sized for use in attitude control of small satellites, for in-orbit testing.
