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The fuel-optimal gravity-assist trajectories are firstly solved using practical variable-specific-impulse solar electrical thrusters. The specific impulse is regarded as a control variable in this case.
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This page is a summary of: Optimization of Variable-Specific-Impulse Gravity-Assist Trajectories, Journal of Spacecraft and Rockets, March 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.a34541.
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