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Comparison of a Field Effect Emission Propulsion System and a Hydrogen Peroxide Monopropellant Thruster for Small Satellites Orbital Control System

Giuseppe Di Pasquale

Comparison of a Field Effect Emission Propulsion System and a Hydrogen Peroxide Monopropellant Thruster for Small Satellites Orbital Control System.

Rel. Lorenzo Casalino. Politecnico di Torino, Corso di laurea magistrale in Ingegneria Aerospaziale, 2019