As part of NASAs lunar exploration Artemis program, the agency is designing a Gateway to orbit8near the moon and provide long term support of a sustained lunar presence at the moon’s south pole.9The first element launched for the Gateway is the Co-Manifested Vehicle (CMV), comprised of the10Power and Propulsion Element (PPE) and Habitation and Lunar Outpost (HALO). The PPE Mission11Design team of McGuire & et. al (2021) has developed a Design Reference Mission (DRM) trajectory12for CMV’s Earth Orbit Raising (EOR) mission phase, which provides the vehicle’s 3 degrees of freedom13(DoF) trajectory information during the approximately yearlong spiral out from low Earth orbit and14into the lunar near-rectilinear halo orbit (NRHO). In tandem, the PPE GN&C team is developing a15high-fidelity and fine temporal resolution 6DoF model of the CMV spacecrafts GN&C performance16for delivery to the Gateway team; this work acts to bridge the gap between Mission Designs 3DoF17reference and detailed GN&Cs attitude simulation.


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    Title :

    Attitude Profile Reference for the Earth Orbit Raising Phase of NASA Gateway’s Co-Manifested Vehicle


    Contributors:
    B. Humphreys (author) / C. Schmid (author) / M. Martini (author) / M. Mcguire (author) / K. Hack (author) / S. Mccarty (author) / M. Holub (author) / N. Tarantino (author) / B. Leiker (author)

    Publication date :

    2022


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Attitude Profile Reference for the Earth Orbit Raising Phase of NASA Gateway’s Co-Manifested Vehicle

    Humphreys, Bradley / Schmid, Christine / Martini, Michael et al. | Springer Verlag | 2024


    PPE Attitude Profile Reference for the Earth Orbit Raising Phase

    Bradley Humphreys / Christine Schmid / Michael Martini et al. | NTRS