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Descripción
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| This paper faces the design of the trajectory of a tether mission to Saturn. To reduce the hyperbolic excess velocity at arrival to the planet, a gravity assist at Jupiter is included. The Earth-to-Jupiter portion of the transfer is unpropelled. The Jupiter-to-Saturn trajectory has two parts: a first coasting arc followed by a second arc where a low thrust engine is switched on. An optimization process provides the law of thrust control that minimizes the velocity relative to Saturn at arrival, thus facilitating the tethered orbit insertion. | |
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Internacional
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Si |
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Nombre congreso
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8th European Conference for Aeronautics and Space Sciences (EUCASS 2019) |
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Tipo de participación
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960 |
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Lugar del congreso
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ETSI Aeronáutica y del Espacio, Universidad Politécnica de Madrid, Madrid, Spain |
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Revisores
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Si |
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ISBN o ISSN
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DOI
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Fecha inicio congreso
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01/07/2019 |
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Fecha fin congreso
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04/07/2019 |
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