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タイトルGalileo 1989 VEEGA trajectory design
著者(英)D'Amario, Louis A.; Johannesen, Jennie R.; Byrnes, Dennis V.; Nolan, Brian G.
著者所属(英)Jet Propulsion Lab., California Inst. of Tech.
発行日1989-09-01
言語eng
内容記述The new baseline for the Galileo Mission is a 1989 Venus-earth-earth gravity-assist (VEEGA) trajectory, which utilizes three gravity-assist planetary flybys in order to reduce launch energy requirements significantly compared to other earth-Jupiter transfer modes. The launch period occurs during October-November 1989. The total flight time is about 6 years, with November 1995 as the most likely choice for arrival at Jupiter. Optimal 1989 VEEGA trajectories have been generated for a wide range of earth launch dates and Jupiter arrival dates. Launch/arrival space contour plots are presented for various trajectory parameters, including propellant margin, which is used to measure mission performance. The accessible region of the launch/arrival space is defined by propellant margin and launch energy constraints; the available launch period is approximately 1.5 months long.
NASA分類ASTRODYNAMICS
レポートNO90A22270
権利Copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/358429


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