Figure 13From: Cluster of electric thrusters for astronautic and robotic INPPS flagship space flights to Mars and Europa moonPlot of necessary PS mass to generate the required thrust including thruster, redundant PPU and PFS over mission time of trajectory Earth-Mars featuring relevant thruster types. Breaks show that required thrust is not achieved with this thruster and therefore another thruster in the CET has to be used during this trajectory sectionBack to article page