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In this chapter several aspects relating to the ᴾᵒCat are described. Do note that these are intended to serve as a reference and may not be representative of your own mission.

In this section an overview the IEEE Open PocketQube is given going into detail of the physical and functional architecture. Spacecraft configuration and radiation measures are also presented.

In this rection requierements for the ᴾᵒCat spacecrafts (system) and corresponding mission are presented. These are to be defined by the team developing each mission and PocketQube.

RFI-5G payload designs. Includes electrical, mechanical and software.