Following a successful tender for European Space Agency funding, the Clean Space One project was redirected towards another target.

Software architecture

* System documentation
* The COM (communication), PL (payload), ADCS (attitude and orientation), and EPS (energy) subsystems all have a MSP430F1611 microcontroller
* The CDMS (on board computer) has an ATMEL ARM AT91M55800A

These microcontrollers used two I²C buses to

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