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.


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    Titel :

    Concurrent engineering: Spacecraft and mission operations system design


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


    Erscheinungsdatum :

    1994-11-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    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

    J. A. Landshof / R. J. Harvey / M. H. Marshall | NTIS | 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


    An Advanced Environment for Spacecraft Engineering Subsystem Mission Operations

    Harris, J. A. / Bahrami, K. A. | SAE Technical Papers | 1992