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Optimization of Refueling Strategies for Electric Propulsion Space Missions

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An evenly distributed refueling sequence maximizes payload mass while optimizing specific impulse.
The study derived analytical expressions for metrics like payload mass and specific propellant consumption.
An optimization problem was formulated to enhance refueling strategies within practical mission time constraints.
Using the SMART-1 mission as a case study, the approach illustrates significant payload increases with longer mission time.

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Analytical framework enhances payload mass and reduces propellant consumption in electric propulsion, suggesting optimal refueling sequences.

Bendimerad et al. (2025) studied this question.

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Analytical framework enhances payload mass and reduces propellant consumption in electric propulsion, suggesting optimal refueling sequences.