This paper examines the potential of aeroassist maneuvers at Mars for missions to the sun and to Pluto, using a high-lift/drag vehicle such as the waverider to perform an atmospheric 'fly-around' of Mars, in order to rotate the planetocentric velocity vector, thus adding to the rather small rotation due to gravity alone. A fly-around in one direction or the other can place the aphelion or the perihelion of the resulting orbit at the Mars distance, for missions toward the sun or toward Pluto, respectively. The parameters of such maneuvers are given as a function of earth launch velocity.


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    Titel :

    Hypersonic maneuvering to provide planetary gravity assist


    Beteiligte:

    Erscheinungsdatum :

    01.01.1990


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Hypersonic maneuvering to provide planetary gravity assist

    MCRONALD, ANGUS / RANDOLPH, JAMES | AIAA | 1990


    Hypersonic maneuvering for augmenting planetary gravity assist

    MCRONALD, ANGUS D. / RANDOLPH, JAMES E. | AIAA | 1992


    Hypersonic maneuvering for augmenting planetary gravity assist

    Mcronald, Angus D. / Randolph, James E. | NTRS | 1992


    Hypersonic Interplanetary Flight: Aero Gravity Assist

    Bowers, Al / Banks, Dan / Randolph, Jim | NTRS | 2006


    SHIP MANEUVERING ASSIST SYSTEM

    HINO TAKENORI / HARADA YOSHITERU / KINUKAWA YUSUKE et al. | Europäisches Patentamt | 2021

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