Research Article

Experimental Approach for the Evaluation of the Performance of a Satellite Module in the CanSat Form Factor for In Situ Monitoring and Remote Sensing Applications

Table 2

Some CubeSat projects and their respective common temperature ranges (maximum and minimum levels), vacuum level, and number of cycles [30].

CubeSatModelT max (°C)T min (°C)Vacuum level (torr)Number of cycle

QB50Proto flight+50-204
Step Cube LabFlight+35-35<10−52
AAU CubeSatFlight+85-10<0.011
Swiss CubeFlight+50-454
NanoSact-BR1Flight+50-102
SERPENSFlight+42-153