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  • On-Orbit Greenhouse Gas Detection with the GHGSat Constellation

    Paper number

    IAC-18,B4,4,8,x47978

    Author

    Ms. Laura Bradbury, Canada, UTIAS Space Flight Laboratory

    Coauthor

    Mr. Michael Ligori, Canada, UTIAS Space Flight Laboratory

    Coauthor

    Mr. Robert Spina, Canada, UTIAS Space Flight Laboratory

    Coauthor

    Mr. Daniel Kekez, Canada, UTIAS Space Flight Laboratory

    Coauthor

    Mr. Pawel Lukaszynski, Canada, Space Flight Laboratory, University of Toronto

    Coauthor

    Dr. Robert Zee, Canada, Space Flight Laboratory, University of Toronto

    Coauthor

    Mr. Stephane Germain, Canada, GHGSat Inc.

    Year

    2018

    Abstract
    Industrial operators are increasingly motivated by regulatory and operational imperatives to quantify their greenhouse gas (GHG) and air quality gas (AQG) emissions with the intent of ultimately reducing them. Utilizing novel satellite technology, GHGSat Inc. intends to become the global leader of greenhouse gas remote sensing. In June 2016, GHGSat-D (Claire) was launched, becoming the first high-resolution microsatellite designed to measure greenhouse gas emissions from point sources, such as industrial facilities and power plants. The bus was provided by the Space Flight Laboratory (SFL) under contract to GHGSat Inc. Claire has successfully demonstrated greenhouse gas measurements around the world, and one such measurement of methane emissions from a hydroelectric dam in Africa was released publicly in early 2017.
    
    In order to extend the service capability and as a precursor to a full constellation, GHGSat-C1 and GHGSat-C2 are the next two microsatellites under development. With a mass of approximately 16 kg each, the design follows its predecessor Claire in leveraging SFL’s Next Generation Earth Monitoring and Observation (NEMO) bus. Bus platform modifications such as enhanced electromagnetic compatibility and hardware redundancy will result in increased performance and reliability. Enhancements to the payload include reduced stray light, onboard calibration capability, and additional radiation mitigation. Furthermore, the inclusion of an optical downlink as a technology demonstrator will result in greater data downlink capacity. These upgrades will be entirely accomplished with the same volume and power constraints as Claire. The development of the GHGSat-C1 and GHGSat-C2 satellites is currently underway and the first of the two is scheduled for launch at the beginning of 2019. This paper describes the mission of the GHGSat constellation and the innovative bus and payload technologies that will enable future development of a full satellite constellation.
    Abstract document

    IAC-18,B4,4,8,x47978.brief.pdf

    Manuscript document

    IAC-18,B4,4,8,x47978.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.