The aim of this project is to analyse the temperature that a 1U CubeSat will encounter on orbit,
and consequently produce a first approach to the thermal design of the satellite Teidesat.
The Microsatellite project team from IACTEC is also petitionary of this bachelor thesis because
they are interested in performing thermal analysis in a CubeSat, so that they can develop their
own nanosatellites. IACTec Microsatellites team is developing the Payload for a 3U CubeSat
mission called ALISIO I, this case will be analysed too.