Micropropulsión basada en combustible sólido - caracterización y aplicación en el control de conservación de órbita en pequeños satélites
Content type: article
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Abstract:
This article presents the work made with the solid propellant micro-thrusters in the MIS group at LAAS-CNRS. In firts 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, specificall missions concerning either individual or a group of small satellites