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  • Development of a Laser Power Beaming Demonstration for CLPS Landers

    Paper number

    IAC-20,C3,2,4,x60799

    Author

    Mr. Ross Centers, United States, Colorado School of Mines

    Coauthor

    Mr. Joshua Schertz, United States, Colorado School of Mines

    Coauthor

    Mr. Curtis Purrington, United States, Colorado School of Mines

    Coauthor

    Mr. David Dickson, United States, Colorado School of Mines

    Coauthor

    Mr. Loren Kezer, United States, Colorado School of Mines

    Coauthor

    Mr. Adam Janikowski, Hong Kong, Colorado School of Mines

    Coauthor

    Mr. John Schmit, United States, Colorado School of Mines

    Coauthor

    Mr. Timofey Broslav, United States, Colorado School of Mines

    Coauthor

    Mr. Jef Hinton, United States, Colorado School of Mines

    Coauthor

    Mr. Leonard D Vance, United States, University of Arizona

    Coauthor

    Mr. Himangshu Kalita, United States, University of Arizona

    Coauthor

    Mr. Alvaro Flores, United States, University of Arizona

    Coauthor

    Mr. Jose Fernandez, United States, University of Arizona

    Coauthor

    Prof. Jekanthan Thangavelautham, United States, University of Arizona

    Coauthor

    Dr. George Sowers, United States, Colorado School of Mines

    Year

    2020

    Abstract
    Laser based power transmission represents an enabling technology for moving power from energy rich regions to areas of high demand, while being able to overcome the dramatic topography of the lunar poles [1-4]. To provide the earliest opportunity for flight demonstration of this critical technology, we have designed and conducted relevant environment testing of a low power, minimal mass laser power beaming demonstrator that can be mounted as an ancillary payload on a NASA Commercial Lunar Payload Services (CLPS) lander. Our entire system consists of a laser, beam director, target identification system, and multiple FemtoSat receivers [5]. This integrated system is able to test key objectives incrementally. We plan to test methods of ejecting and locating the receiver on the lunar surface, pointing and aiming the laser at the receiver, and powering the receiver. We have tested key components of the system and are moving toward integrated tests.
    Abstract document

    IAC-20,C3,2,4,x60799.brief.pdf

    Manuscript document

    IAC-20,C3,2,4,x60799.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.