The application of a nuclear electric propulsion (NEP) stage in the exploration of near-earth, cometary, and planetary space was discussed. The NEP stage is powered by a liquid-metal-cooled, fast spectrum thermionic reactor capable of providing 120 kWe for 20,000 hours. This power is used to drive a number of mercury ion bombardment thrusters with specific impulse in the range of 4000-5000 seconds. The NEP description, characteristics, and functional requirements are discussed. These requirements are based on a set of five coordinate missions, which are described in detail. These five missions are a representative part of a larger set of missions used as a basic for an advanced propulsion comparison study. Additionally, the NEP stage development plan and test program is outlined and a schedule presented.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Nuclear electric propulsion stage requirements and description


    Beteiligte:
    Mondt, J. F. (Autor:in) / Peelgren, M. L. (Autor:in) / Nakashima, A. M. (Autor:in) / Nsieh, T. M. (Autor:in) / Phillips, W. M. (Autor:in) / Kikin, G. M. (Autor:in)

    Erscheinungsdatum :

    1974-08-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Nuclear Electric Propulsion Stage Requirements and Description

    J. F. Mondt / M. L. Peelgren / A. M. Nakashima et al. | NTIS | 1974


    Multi-mission nuclear electric propulsion stage design.

    Prickett, W. Z. / Stearns, J. W. | NTRS | 1973


    SDIO ELECTRIC PROPULSION REQUIREMENTS

    Vondra, R. J. / Caveny, L. H. / United States | British Library Conference Proceedings | 1990



    SDIO Electric Propulsion Requirements

    R. J. Vondra / L. H. Caveny | NTIS | 1990