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  • INPPS Flagship: Cluster of Electric Thrusters

    Paper number

    IAC-19,C4,4,11,x52152

    Author

    Dr. Frank Jansen, Germany, DLR (German Aerospace Center)

    Coauthor

    Dr. Tim Brandt, Czech Republic, CTU in Prague

    Coauthor

    Dr. Emmanouil Detsis, France, European Science Foundation (ESF)

    Coauthor

    Dr. Athanasios Dafnis, Germany, RWTH Aachen University - Institut fuer Leichtbau

    Coauthor

    Mrs. Simona Ferraris, Italy, Thales Alenia Space Italia

    Coauthor

    Mr. James AP Findlay, United Kingdom, National Nuclear Laboratory

    Coauthor

    Dr. Ikkoh Funaki, Japan, JAXA/ISAS

    Coauthor

    Dr. Richard Granjon, France, Sagem Defence and Security

    Coauthor

    Mr. Jan Thimo Grundmann, Germany, DLR (German Aerospace Center)

    Coauthor

    Dr. Gerhard Grunwald, Germany, DLR (German Aerospace Center)

    Coauthor

    Dr. Lamartine Nogueira Frutuoso Guimaraes, Brazil, Instituto de Estudos Avancados

    Coauthor

    Mr. Martin Hillebrandt, Germany, Deutsch Luft und Raumfahrt Zentrum (DLR)

    Coauthor

    Prof. A.C. Koroteev, Russian Federation, Keldych Research Centre

    Coauthor

    Dr. Jim C. Kuijper, The Netherlands

    Coauthor

    Dr. Francois Lassoudiere, France, Airbus Safran Launchers

    Coauthor

    Mr. Masson Frederic, France

    Coauthor

    Dr. Michel Muszynski, France, Airbus Safran Launchers

    Coauthor

    Mr. Stephane Oriol, France, Centre National d'Etudes Spatiales (CNES)

    Coauthor

    Mr. Martin Richter, Germany, DLR (German Aerospace Center)

    Coauthor

    Dr. Lars Schanz, Germany, DLR (German Aerospace Center)

    Coauthor

    Dr. Alexander V. Semenkin, Russian Federation, Keldych Research Centre

    Coauthor

    Dr. Alexander E. Solodukin, Russian Federation

    Coauthor

    Mr. Tim Tinsley, United Kingdom, National Nuclear Laboratory

    Coauthor

    Dr. Maria Cristina Tosi, Italy, Thales Alenia Space

    Coauthor

    Dr. Jean-Claude Worms, France, European Science Foundation

    Year

    2019

    Abstract
    This paper describes the results of the European-Russian DEMOCRITOS and MEGAHIT projects related to the electric thrusters on board the International Nuclear Power and Propulsion System (INPPS) flagship. INPPS flagship is a high power space transportation hybrid tug (power supply primary by nuclear power, by auxiliary solar power ring and chemical propulsion due to subsystems transport for assembly at high Earth orbit above 800 km) for Mars, Europa, Moon and asteroid exploration flights.
    
    In dependence from the actual exploration mission, mission phases / trajectory and preferred international high power electric thrusters (about 20 - 50 kW) with different specific impulse, the results will be discussed in detail - also as a function of the transportable payload mass. Because of the 1 MWel nuclear reactor (successful test confirmed by Russia in 2018) as  the power supply for INPPS a cluster of about 15 electric thrusters was studied in DEMOCRITOS project for MARS and EUROPA INPPS flagships. Issues related to power processing units for the electric thrusters were identified and will be discussed. In addition low power (kW) thrusters for an INPPS flagship orbiting small inspection satellite are sketched too. 
    
    Insofar the presentation is directly highlighting aspects of disruptive electric propulsion subsystems, within INPPS space system and applied to visionary Mars (including non-human and human) and Europa exploration and space transport tug flights.
    Abstract document

    IAC-19,C4,4,11,x52152.brief.pdf

    Manuscript document

    IAC-19,C4,4,11,x52152.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.