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  • Thermo-mechanical design for a miniaturized quantum light source on board the SpooQy-1 CubeSat

    Paper number

    IAC-21,B4,6B,5,x64681

    Author

    Ms. Huai Ying Lim, Singapore, Republic of, SpeQtral

    Coauthor

    Mr. Tom Vergoossen, Singapore, Republic of, SpeQtral

    Coauthor

    Dr. Robert Bedington, Singapore, Republic of

    Coauthor

    Mr. Xueliang Bai, Australia, The University of Sydney

    Coauthor

    Dr. Aitor Villar, Singapore, Republic of, SpeQtral

    Coauthor

    Dr. Alexander Lohrmann, Singapore, Republic of, SpeQtral

    Coauthor

    Ms. Hong-Nhung Nguyen, Singapore, Republic of, National University of Singapore

    Coauthor

    Dr. Alexander Ling Euk Jin, Singapore, Republic of

    Coauthor

    Mr. Simon Barraclough, Australia, UNSW Australia

    Coauthor

    Mr. Jai Vennik, Australia, University of New South Wales

    Coauthor

    Dr. Douglas Griffin, Australia, Australian Defence Force Academy (ADFA)

    Year

    2021

    Abstract
    This paper presents the thermo-mechanical design of the quantum light source on board SpooQy-1, a 3U CubeSat that was deployed from the International Space Station on 17th June 2019. SpooQy-1 is a technology demonstrator for space-based quantum networks. The on-board light source generates and detects polarization-entangled photon pairs to validate its in-orbit performance. Entangled photons are generated using spontaneous parametric down-conversion (SPDC) necessitating stringent dimensional stability and temperature requirements. Under laboratory conditions these requirements are routinely met using off-the-shelf laboratory mounts and alignment mechanisms. However, when facing harsh environments such as the vibration during rocket launch or temperature changes due to fluctuating illumination conditions, custom thermo-mechanical solutions are required. In this work, the development and in-orbit demonstration of an isostatic payload mount is discussed. This mounting approach enables future space missions with quantum instruments on resource-constrained CubeSat platforms with limited thermal control capabilities.
    Abstract document

    IAC-21,B4,6B,5,x64681.brief.pdf

    Manuscript document

    (absent)