Abstract
This study investigates the feasibility of a Moon-enabled Sun occultation mission to observe the solar corona, normally obscured by the Sun's brightness. The concept involves positioning a spacecraft behind the Moon to block the incident light coming from the solar disk. Low-thrust propulsion is analyzed to assess its suit-ability for such a mission. The mission geometry includes lunar flybys to modify the orbit, enabling the spacecraft to pass through designated occultation zones. A multi-arc approach is employed to optimize the full trajectory while accounting for mission constraints.