Historically, the Mission Operations System (MOS) for a space mission has been designed last because it is needed last. This has usually meant that the ground system must adjust to the flight vehicle design, sometimes at a significant cost. As newer missions have increasingly longer flight operations lifetimes, the MOS becomes proportionally more difficult and more resource-consuming. We can no longer afford to design the MOS last. The MOS concept may well drive the spacecraft, instrument, and mission designs, as well as the ground system. A method to help avoid these difficulties, responding to the changing nature of mission operations is presented. Proper development and use of an Operations Concept document results in a combined flight and ground system design yielding enhanced operability and producing increased flexibility for less cost.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Operations Concept Methodology to Achieve Low-Cost Mission Operations


    Beteiligte:
    K. W. Ledbetter (Autor:in) / S. D. Wall (Autor:in)

    Erscheinungsdatum :

    1993


    Format / Umfang :

    6 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    An operations concept methodology to achieve low-cost mission operations

    Ledbetter, Kenneth W. / Wall, Stephen D. | NTRS | 1993


    Operations concept for TES mission operations

    Varanasi, P. / Tyler, S. | IEEE | 2002


    Space Mission Operations Concept

    Squibb, G. F. | NTRS | 1996


    Shared mission operations concept

    Spradlin, Gary L. / Rudd, Richard P. / Linick, Susan H. | NTRS | 1994


    12.0401 Operations Concept for TES Mission Operations

    Institute of Electrical and Electronics Engineers | British Library Conference Proceedings | 2002