The trajectory and mission design process in cislunar space can benefit from multibody dynamical systems approaches. This two-part webinar will explore such concepts and discussion focused on the first Earth-Moon libration point mission, ARTEMIS (the follow-up to THEMIS), followed by introducing a rapid prototyping tool.
Venue:
Virtual
The trajectory and mission design process in cislunar space can benefit from multibody dynamical systems approaches. Indeed, many current and upcoming missions leverage these strategies. This two-part webinar will explore such concepts and will begin with a motivating discussion focused on the first Earth-Moon libration point mission, ARTEMIS (the follow-up to THEMIS), followed by the introduction of a rapid prototyping tool intended to facilitate design strategies quickly, the Cislunar Orbit Designer (CODE).
