respectively2. The orbit of Dimorphos around Didymos before the impact, depicted by the black circle, has a semimajor axis of 1.206 ± 0.035 km3and an eccentricity of <0.03
In this context, a reference CubeSat configuration is assumed to obtain some sort of nominal transfer performance values for comparison purposes. In this regard, the reference CubeSat has a single BIT-3 RF ion thruster unit. In other words, the characteristics of the reference CubeSat are similar...