  Numerous high-thrust and low-thrust space propulsion technologies have been
developed in the recent years with the goal of expanding space exploration
capabilities; however, designing and optimizing a multi-mission campaign with
both high-thrust and low-thrust propulsion options are challenging due to the
coupling between logistics mission design and trajectory evaluation.
Specifically, this computational burden arises because the deliverable mass
fraction (i.e., final-to-initial mass ratio) and time of flight for low-thrust
trajectories can can vary with the payload mass; thus, these trajectory metrics
cannot be evaluated separately from the campaign-level mission design. To
tackle this challenge, this paper develops a novel event-driven space logistics
network optimization approach using mixed-integer linear programming for space
campaign design. An example case of optimally designing a cislunar propellant
supply chain to support multiple lunar surface access missions is used to
demonstrate this new space logistics framework. The results are compared with
an existing stochastic combinatorial formulation developed for incorporating
low-thrust propulsion into space logistics design; our new approach provides
superior results in terms of cost as well as utilization of the vehicle fleet.
The event-driven space logistics network optimization method developed in this
paper can trade off cost, time, and technology in an automated manner to
optimally design space mission campaigns.
