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  • Demonstrating miniaturised, entangled photon-pair sources on board nanosatellites to enable future QKD missions.

    Paper number

    IAC-17,B2,7,2,x38915

    Author

    Dr. Rakhitha Bandara Chandrasekara, National University of Singapore, Singapore, Republic of

    Coauthor

    Dr. Robert Bedington, National University of Singapore, Singapore, Republic of

    Coauthor

    Dr. Xueliang Bai, National University of Singapore, Singapore, Republic of

    Coauthor

    Mr. Tang Zhongkan Xavier, National University of Singapore, Singapore, Republic of

    Coauthor

    Mr. Sean Yau, National University of Singapore, Singapore, Republic of

    Coauthor

    Dr. Tanvirul Islam, National University of Singapore, Singapore, Republic of

    Coauthor

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

    Coauthor

    Dr. Douglas Griffin, University of New South Wales ADFA, Australia

    Coauthor

    Mr. Denis Naughton, University of New South Wales, Australia

    Coauthor

    Mr. Simon Barraclough, UNSW Australia, Australia

    Coauthor

    Prof. Russell Boyce, University of New South Wales ADFA, Australia

    Coauthor

    Dr. Alexander Ling Euk Jin, Singapore, Republic of

    Year

    2017

    Abstract
    We report on our progress developing highly-miniaturised, polarisation-entangled, photon-pair sources for CubeSats. We have a correlated photon source in orbit in the NUS Galassia 2U CubeSat. We also have an entangled photon-pair source in production and a high brightness (~1Mcps) entangled photon-pair source in development for our upcoming CQT SpooQySat  3U CubeSats. All our sources are proof-of-principle demonstrations that the hardware necessary for entanglement-based QKD can be miniaturised and made sufficiently robust for operation in nanosatellites. The photon pairs they produce are measured with liquid crystal-based Bell state analysers and geiger-mode avalanche photo-diodes onboard the source. These space missions allow our on-the-ground radiation, thermal and vibration tests to be validated and the real-world operation and aging of the source in space to be studied. A BBM92 QKD-capable design of the source has been used in a phase A study of a satellite-to-satellite QKD demonstration mission by the University of New South Wales, Canberra. This mission study uses two 6U CubeSats in LEO and aims to demonstrate QKD over separations of increasing distances as the two CubeSats drift apart.
    Abstract document

    IAC-17,B2,7,2,x38915.brief.pdf

    Manuscript document

    IAC-17,B2,7,2,x38915.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.