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Low-energy transfers are important to design trajectories visiting two or more moons in a planetary system. We propose new multi-burn strategies with variable intermediate arcs in the framework based on Moon-to-Moon Analytical Transfer (MMAT) to achieve propellant saving.
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This page is a summary of: Flexible Bridge-Conic Strategies for Moon-to-Moon Analytical Transfer Design, Journal of Spacecraft and Rockets, October 2024, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a36156.
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