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  • Compact Aneutronic Fusion Propulsion

    Paper number

    IAC-12,C4,7-C3.5,10,x15548

    Author

    Mr. Michael Paluszek, Princeton Satellite Systems, United States

    Coauthor

    Mr. Yosef Razin, Princeton Satellite Systems, United States

    Coauthor

    Dr. Gary Pajer, Princeton Satellite Systems, United States

    Coauthor

    Dr. Samuel Cohen, Princeton Plasma Physics Laboratory, United States

    Coauthor

    Ms. Mary Breton, United States

    Coauthor

    Mr. Joseph Mueller, United States

    Coauthor

    Mr. Eric Ham, United States

    Coauthor

    Dr. A. H. Glasser, University of Washington, United States

    Year

    2012

    Abstract
    This paper presents the design of a compact aneutronic fusion engine which will enable more challenging exploration missions in the solar system. The engine uses  a Deuterium-Helium-3 reaction  to produce fusion energy. The Deuterium-Helium-3  reaction requires a temperature three times greater than a Deuterium-Tritium (D-T) reaction but  produces much lower levels of neutrons than a D-T reaction. Lower neutron levels reduce the needed shielding and also reduces the waste energy unavailable for propulsion. The engine employs a field reversed magnetic field configuration (FRC) and a novel radio-frequency heating system. The FRC has a relatively simple linear solenoidal coil configuration yet permits higher plasma pressures for a given magnetic field than other designs. Waste heat generated from bremsstrahlung and synchrotron radiation can be recycled to maintain the fusion temperature. The charged reaction products are exhausted directly for propulsion through a magnetic nozzle. The heating scheme only works for reactors with radii less than 0.5 hence the optimal size for each engine is between 5 and 10 MW. The paper provides a system design of the engine. Analysis of electrical power generation, thermal management and magnetic coil subsystems are included. Results are presented for the Jupiter Icy Moon Orbiter Mission and a manned Mars mission.
    Abstract document

    IAC-12,C4,7-C3.5,10,x15548.brief.pdf

    Manuscript document

    IAC-12,C4,7-C3.5,10,x15548.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.