This document contains the deliverables for the NASA Research and Technology for Aerospace Propulsion Systems (RTAPS) regarding the stability, transient response, control, and safety study for a high power cryogenic turboelectric distributed propulsion (TeDP) system. The objective of this research effort is to enumerate, characterize, and evaluate the critical issues facing the development of the N3-X concept aircraft. This includes the proposal of electrical grid architecture concepts and an evaluation of any needs for energy storage.


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    Titel :

    Stability, Transient Response, Control, and Safety of a High-Power Electric Grid for Turboelectric Propulsion of Aircraft


    Beteiligte:
    M. Armstrong (Autor:in) / C. Ross (Autor:in) / D. Phillips (Autor:in) / M. Blackwelder (Autor:in)

    Erscheinungsdatum :

    2013


    Format / Umfang :

    140 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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