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
