Despite our awareness of the mission design process, spacecraft historically have been designed and developed by one team and then turned over as a system to the Mission Operations organization to operate on-orbit. By applying concurrent engineering techniques and envisioning operability as an essential characteristic of spacecraft design, tradeoffs can be made in the overall mission design to minimize mission lifetime cost. Lessons learned from previous spacecraft missions will be described, as well as the implementation of concurrent mission operations and spacecraft engineering for the Near Earth Asteroid Rendezvous (NEAR) program.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Concurrent Engineering: Spacecraft and Mission Operations System Design


    Beteiligte:
    J. A. Landshof (Autor:in) / R. J. Harvey (Autor:in) / M. H. Marshall (Autor:in)

    Erscheinungsdatum :

    1994


    Format / Umfang :

    7 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Concurrent Engineering: Spacecraft and Mission Operations System Design

    Landshof, J. A. / Harvey, R. J. / Marshall, M. H. et al. | British Library Conference Proceedings | 1994


    Concurrent engineering: Spacecraft and mission operations system design

    Landshof, J. A. / Harvey, R. J. / Marshall, M. H. | NTRS | 1994


    Spacecraft and Mission Design of the Arenas Mercury Orbiter Using Methods of Concurrent Engineering

    Joseph, S. M. / Flowers-Jacobs, N. E. / Humpherey, F. et al. | British Library Conference Proceedings | 2000



    Spacecraft and mission design of the 'Aeneas' Mercury orbiter using methods of concurrent engineering

    Joseph, S.M. / Flowers-Jacobs, N.E. / Jackson, R.P. et al. | IEEE | 2000