After completion of a resupply mission to NASA's proposed Lunar Orbital Platform - Gateway, safe disposal of the Logistics Module is required. One potential option is disposal to heliocentric space. This investigation includes an exploration of the trajectory escape dynamics from an Earth-Moon Near Rectilinear Halo Orbit (NRHO) and applies these insights to the design of a low-cost heliocentric Logistics Module disposal option. The effects of the solar gravitational perturbations are assessed in both the bicircular restricted 4-body problem and in an ephemeris force model.


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    Titel :

    Disposal Trajectories from Near Rectilinear Halo Orbits


    Beteiligte:

    Kongress:

    AAS/AIAA Astrodynamics Specialists Conference ; 2018 ; Snowbird, UT, United States


    Erscheinungsdatum :

    2018-08-19


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Disposal, Deployment, and Debris in Near Rectilinear Halo Orbits

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    Disposal, Deployment, and Debris in Near Rectilinear Halo Orbits

    Davis, Diane C. / Boudad, Kenza K. / Phillips, Sean M. et al. | NTRS | 2019


    Jettison and Disposal from Near Rectilinear Halo Orbits, Part 1: Theory

    Stephen T. Scheuerle / Diane C. Davis / Emily M. Zimovan-Spreen et al. | NTRS


    Jettison and Disposal From Near Rectilinear Halo Orbits, Part 2: Applications

    Diane C. Davis / Stephen T. Scheuerle / Steven L. McCarty et al. | NTRS