Objects deployed from a Near Rectilinear Halo Orbit (NRHO) experience simultaneous gravitational forces from the Moon, the Earth, and the Sun, and post-deployment behavior is complex. The current investigation applies the theories explored in Part 1 of the study to examine the dynamics of objects deployed from the Gateway NRHO to heliocentric space. Examples include jettison of cubesats and logistics modules as well as end-of-life options for the Gateway itself. Recontact risk with the Gateway as each object departs the lunar vicinity is explored, and both the immediate destination and the long-term fate of the deployed objects are assessed.


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    Titel :

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


    Beteiligte:

    Kongress:

    AAS/AIAA Astrodynamics Specialist Conference ; 2023 ; Big Sky, MT, US


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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

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


    Disposal Trajectories from Near Rectilinear Halo Orbits

    Boudad, Kenza K. / Davis, Diane C. / Howell, Kathleen C. | NTRS | 2018


    Disposal, Deployment, and Debris in Near Rectilinear Halo Orbits

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


    Disposal, Deployment, and Debris in Near Rectilinear Halo Orbits

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


    Eigenmotion Control for Near Rectilinear Halo Orbits

    WEISS AVISHAI / ELANGO PURNANAND / DI CAIRANO STEFANO et al. | Europäisches Patentamt | 2023

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