NASA is providing preliminary design and requirements for the Space Launch System Exploration Upper Stage (EUS). The EUS will provide upper stage capability for vehicle ascent as well as on-orbit control capability. Requirements include performance of on-orbit burn to provide Orion vehicle with escape velocity. On-orbit attitude control is accommodated by a on-off Reaction Control System (RCS). Paper provides overview of approaches for design and stability of an attitude control system using a RCS.


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    Titel :

    Design and Stability of an On-Orbit Attitude Control System Using Reaction Control Thrusters


    Beteiligte:
    R. A. Hall (Autor:in) / S. Hough (Autor:in) / C. Orphee (Autor:in) / K. Clements (Autor:in)

    Erscheinungsdatum :

    2016


    Format / Umfang :

    18 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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