Satellites deployed from the Gateway in a Near Rectilinear Halo Orbit (NRHO) must be safely delivered their desired destinations in cislunar space and beyond. The presence of simultaneously significant gravitational forces from the Moon, the Earth, and the Sun, along with the absence of atmospheric drag, complicates the mission design problem for cubesats deployed from the Gateway. The current investigation defines candidate green zones for safe satellite deployment, allowing a passive departing spacecraft to avoid recontact with the Gateway as it departs the NRHO vicinity.


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    Titel :

    Cubesat Deployment from a Near Rectilinear Halo Orbit


    Beteiligte:

    Kongress:

    32nd AIAA/AAS Spaceflight Mechanics Meeting ; 2022 ; San Diego, CA, US


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Cubesat Deployment from a Near Rectilinear Halo Orbit

    Davis, Diane C. / Zimovan-Spreen, Emily M. / Power, Rolfe J. et al. | AIAA | 2022


    Cubesat Deployment from a Near Rectilinear Halo Orbit

    Davis, Diane C. / Zimovan-Spreen, Emily M. / Power, Rolfe J. et al. | TIBKAT | 2022


    Cubesat Deployment from a Near Rectilinear Halo Orbit

    D. C. Davis / E. M. Zimovan-Spreen / R. J. Power et al. | NTIS | 2021


    Baseline Orbit Generation for Near Rectilinear Halo Orbits

    Emily M. Zimovan-Spreen / Stephen T. Scheuerle / Brian P. Mccarthy et al. | NTRS


    Using GNSS Receiver at Near Rectilinear Halo Orbit

    Nakajima, Yu / Yamamoto, Toru / Ikeda, Hitoshi | TIBKAT | 2019