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Descripción
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| We present the design of a low-thrust trajectory to Saturn with a gravity assist at Jupiter. In the Earth-to- Jupiter portion of the transfer, the propulsion system applies constant thrust in the direction of the orbital velocity to increase the semimajor axis at the fastest rate. After the swingby, the thruster is fired during a portion of the Jupiter-to-Saturn transfer and implements a steering law that minimizes the velocity relative to Saturn at arrival, thus facilitating the orbit insertion | |
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Internacional
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Si |
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JCR del ISI
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No |
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Título de la revista
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8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND AEROSPACE SCIENCES (EUCASS) |
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ISSN
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Factor de impacto JCR
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Información de impacto
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Volumen
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DOI
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Número de revista
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Desde la página
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1 |
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Hasta la página
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11 |
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Mes
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SIN MES |
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Ranking
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