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    NASA Double Asteroid Redirection Test (Dart) Trajectory Validation and Robustness

    NASA Double Asteroid Redirection Test (Dart) Trajectory Validation and Robustness


    The Double Asteroid Redirection Test (DART) mission will be the first to test the concept of a kinetic impactor. Several studies have been made on asteroid redirection and impact mitigation, however, to this date no mission tested the proposed concepts. An impact study on a representative body allows the measurement of the effects on the target's orbit and physical structure. With this goal, DART's objective is to verify the effectiveness of the kinetic impact concept for planetary defense. The spacecraft uses solar electric propulsion to escape Earth, flyby (138971) 2001 CB21 for impart rehearsal, and impact the secondary body of the (65803) Didymos system. This work focuses on the interplanetary trajectory design part of the mission with the validation of the baseline trajectory, performance comparison to other mission objectives, and assessment of the baseline robustness to missed thrust events. Results show a good performance of the selected trajectory for different mission objectives: latest possible escape date, maximum kinetic energy on impact, shortest possible time of flight, and use of an Earth swing-by. The baseline trajectory was shown to be robust to a missed thrust with 1% of fuel margin being enough to recover the mission for failures of more than 14 days.

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    Titel :

    NASA Double Asteroid Redirection Test (Dart) Trajectory Validation and Robustness

    Beteiligte:
    Sarli, Bruno V. (Autor:in) / Ozimek, Martin T. (Autor:in) / Atchison, Justin A. (Autor:in) / Englander, Jacob A. (Autor:in) / Barbee, Brent W. (Autor:in)
    Kongress:

    AAS/AIAA Space Flight Mechanics Meeting ; 2017 ; San Antonio, TX, United States

    Erscheinungsdatum :

    2017-02-05

    Medientyp :

    Aufsatz (Konferenz)

    Format :

    Keine Angabe

    Sprache :

    Englisch

    Schlagwörter :

    Astrodynamics , Lunar And Planetary Science And Exploration , optimization , trajectory , design

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