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  • Laser wireless power transmission system for the spacecraft: design and testing of the prototype

    Paper number

    IAC-14,C3,2,8,x25819

    Author

    Mr. Ivan Matsak, S.P. Korolev Rocket and Space Corporation Energia, Russian Federation

    Coauthor

    Dr. Roman Evdokimov, S.P. Korolev Rocket and Space Corporation Energia, Russian Federation

    Coauthor

    Mr. Vitaliy Kapranov, S.P. Korolev Rocket and Space Corporation Energia, Russian Federation

    Coauthor

    Ms. Tatiana Nikitina, S.P. Korolev Rocket and Space Corporation Energia, Russian Federation

    Coauthor

    Dr. Vjatcheslav Tugaenko, S.P. Korolev Rocket and Space Corporation Energia, Russian Federation

    Coauthor

    Ms. Olga Zayats, S.P. Korolev Rocket and Space Corporation Energia, Russian Federation

    Year

    2014

    Abstract
    Wireless power transmission is considered as promising technology for space application in medium and long term. During 4 years the technology has passed through successive stages from basic principles to prototype demonstration 
    Two test of prototype were carried out for the technology readiness level demonstration. 100 and 1000 meters wireless power transmission experiment were performed. 100 W of optical power was transmitted to static and dynamic receivers with subsequent storage in the li-ion battery. The unmanned aerial vehicle and rover with fixed laser power converter were used as moving targets. 
    The key components of the prototype are: 810 mn diode laser, off-axis beam forming system, GaAs high efficiency laser power converter and fine guidance system. Depending on guidance precision the efficiency of power transmission was in range from 5 to 12\%. Technology readiness level was proved as TRL 6. 
    The next step of technology demonstration is ISS based experiment. Design of stringent requirements equipment for power transmission from ISS to transport cargo vehicles is being performed. 
    In this paper the laser wireless power experiment and evaluation of prototype characteristic are described.
    Abstract document

    IAC-14,C3,2,8,x25819.brief.pdf

    Manuscript document

    (absent)