Power supply design for unmanned electric propulsion missions to outer planets utilizes a store of curium-244 in compact array of capsules as energy source. Supply subassemblies are: heat source, converter equipment which supplies power, and safety equipment. System is designed for a 72,000 hour mission.


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    Titel :

    Radioisotope thermionic power supply for spacecraft


    Beteiligte:
    Homeyer, W. G. (Autor:in) / Gietzen, A. J. (Autor:in) / Heath, C. A. (Autor:in)

    Erscheinungsdatum :

    1972-05-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Nuclear thermionic power system for spacecraft

    Phillips, W.M. / Eastabrook, W.C. / Hsieh, T.M. | Tema Archiv | 1976


    Radioisotope AMTEC power system designs for spacecraft applications

    Ivanenok, J.F. / Sievers, R.K. / Hunt, T.K. et al. | IEEE | 1993


    Saturn Spacecraft Power: Trading Radioisotope, Solar, and Fission Power Systems

    Oleson, Steven R. / Kohout, Lisa / Lorenz, Ralph | AIAA | 2016



    Utilizing Radioisotope Power System Waste Heat for Spacecraft Thermal Management

    Pantano, David / Dottore, Frank / Tobery, E. et al. | AIAA | 2005