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This is a graduate textbook on the theory and applications of optimal spacecraft trajectories. Primarily, this means using the minimum amount of propellant possible to reach a target destination. The author aims to produce the only comprehensive treatment of various aspects of this topic.
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This is a graduate textbook on the theory and applications of optimal spacecraft trajectories. Primarily, this means using the minimum amount of propellant possible to reach a target destination. The author aims to produce the only comprehensive treatment of various aspects of this topic.