![]() ![]() These were grouped according to the dependence of the treatments formulated in thermal and dynamic variables. For the above, two experimental units were used, and all the performance variables of the different satellite subsystems were discriminated against. ![]() For the above, two experimental units were used, and all the performance variables of the different satellite subsystems were discriminated. To evaluate its performance and ensure the precision and accuracy of the measurements made by the satellite prototype, a methodology was designed and implemented for the characterization and qualification of CanSats (soda can satellites) through statistical tests and techniques of DoE (Design of Experiments) based on CubeSat aerospace standards and regulations, in the absence of official test procedures for these kinds of satellite form factor. This article includes the phases of conceptualization and validation of a picosatellite prototype named Simple-2 for remote sensing activities using COTS (Commercial-Off-The-Shelf) components and the modular design methodology.
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