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  • Optical Networks in LEO Based on the CubeSat Standard

    Paper number

    IAC-18,B2,7,3,x45165

    Author

    Dr. Richard Welle, United States, The Aerospace Corporation

    Year

    2018

    Abstract
    The advent of small laser transmitters, in combination with highly-capable CubeSats incorporating precision attitude
    control, enables the development of optical communications networks in Low Earth Orbit (LEO) based entirely in
    satellites built to the CubeSat standard.  This paper will report on development and on-orbit testing of a laser
    downlink from a 1.5U CubeSat in the NASA-funded Optical Communication and Sensor Demonstration (OCSD) Mission that
    launched in November 2017.  The laser transmitter developed for this demonstration has a volume of 250 $\rm{cm^3}$, a mass
    of 360 g, and will produce a 3 W optical output with an input power under 15 W. All of these requirements can easily
    be accommodated in a CubeSat as small as 1.5U. In OCSD, which includes two separate flight units, the two lasers
    are configured for experimental purposes with beam divergences of 0.15 degrees and 0.05 degrees, supporting downlink
    rates of up to 200 Mb/s.  Continuing improvements in pointing capability will allow the laser beam divergence to
    be reduced in future iterations, ultimately supporting data rates well into the Gb/s range.  The OCSD technology
    demonstration mission is expected to complete testing by the middle of 2018. Because of long delays in the
    launch of OCSD, this demonstration mission leads planned implementation of operational laser downlinks in future
    CubeSat missions by only a few months. 
    
    Although the OCSD mission is configured only for downlinks, it has been used as a baseline for designing
    a 3U CubeSat optical crosslink demonstration mission expected to be capable of Gb/s data rates out to 5000
    km range.  Basing an optical relay satellite on the CubeSat standard, particularly smaller CubeSats, allows
    the cost of even very large constellations to be quite modest. This approach would enable a very rapid growth in
    the number of satellite nodes, as would be required over the long term to develop an in-space internet approaching
    the magnitude of the terrestrial internet.  Beyond the development of the basic laser downlink capability, Aerospace
    has been investigating several technologies required to support development of large-scale LEO CubeSat relay
    networks including simple bent-pipe optical relays, agile communication nodes capable of receiving and transmitting
    multiple beams, and the control algorithms required to manage such complex networks.  The results of the
    combined on-orbit experiments, next-generation relay satellite designs, and analyses of control systems indicate
    that CubeSat-scale satellites can have a significant role to play in the development of future large-scale in-space
    internet capabilities.
    Abstract document

    IAC-18,B2,7,3,x45165.brief.pdf

    Manuscript document

    IAC-18,B2,7,3,x45165.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.