Gustavo Adolfo Ardila RodríguezCarole RossiFernando Jiménez2026-03-222026-03-22200410.16924/revinge.19.2https://doi.org/10.16924/revinge.19.2https://andeanlibrary.org/handle/123456789/64679This article presents the work made with the solid propellant micro-thrusters in the MIS group (Microsystems and Systems Integration) at LAAS-CNRS (Laboratory for Analysis and Architecture of Systems) located in Toulouse (France). In first place the ignition process and thrust level were characterized, then, in a second part, its applicability over the station keeping of spatial missions was evaluated, specifically missions concerning either individual or a group (constellation) of small satellites (microsatellites, nano-satellites).esPropellantConstellationGeographyAerospace engineeringAeronauticsHumanitiesEnvironmental scienceEngineeringarticle