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  • SOAR -- A Satellite for Orbital Aerodynamics Research

    Paper number

    IAC-18,B4,2,2,x43107

    Author

    Dr. Nicholas H. Crisp, United Kingdom, The University of Manchester

    Coauthor

    Dr. Peter C.E. Roberts, United Kingdom, The University of Manchester

    Coauthor

    Dr. Steve Edmondson, United Kingdom, The University of Manchester

    Coauthor

    Dr. Sarah Haigh, United Kingdom, The University of Manchester

    Coauthor

    Ms. Sabrina Livadiotti, United Kingdom, The University of Manchester

    Coauthor

    Mrs. Rachel Lyons, United Kingdom

    Coauthor

    Dr. Vitor Oiko, United Kingdom, The University of Manchester

    Coauthor

    Dr. Katharine Smith, United Kingdom, University of Manchester

    Coauthor

    Dr. Stephen Worrall, United Kingdom, The University of Manchester

    Coauthor

    Dr. Jonathan Becedas Rodríguez, Spain, Elecnor Deimos

    Coauthor

    Mr. Gerardo González, Spain, Elecnor Deimos Satellite Systems

    Coauthor

    Ms. Rosa María Domínguez, Spain, Elecnor Deimos Satellite Systems

    Coauthor

    Mr. Leonardo Ghizoni, Denmark, GomSpace ApS

    Coauthor

    Mr. Victor Jungnell, Denmark, GomSpace ApS

    Coauthor

    Mr. Kristian Bay, Denmark, GomSpace ApS

    Coauthor

    Dr. Jonas Morsbøl, Denmark, GomSpace ApS

    Coauthor

    Dr. Georg H. Herdrich, Germany, University of Stuttgart

    Coauthor

    Mr. Francesco Romano, Germany, Institute of Space Systems, Universität Stuttgart

    Coauthor

    Mr. Tilman Binder, Germany, University of Stuttgart

    Coauthor

    Mr. Adam Boxberger, Germany, IRS, University of Stuttgart

    Coauthor

    Prof. Stefanos Fasoulas, Germany, University of Stuttgart

    Coauthor

    Dr. Daniel Garcia-Almiñana, Spain, UPC-BarcelonaTECH

    Coauthor

    Dr. Silvia Rodriguez-Donaire, Spain, UPC-BarcelonaTECH

    Coauthor

    Dr. Miquel Sureda, Spain, UPC-BarcelonaTECH

    Coauthor

    Dr. Dhiren Kataria, United Kingdom, University College London (UCL)

    Coauthor

    Prof. Ronald Outlaw, United States, Mason School of Business, College of William and Mary

    Coauthor

    Dr. Mark Davidson, United States, The Tech Toybox

    Coauthor

    Ms. Rachel Villain, France, Euroconsult

    Coauthor

    Mr. Jose Santiago Perez Cano, France, Euroconsult

    Coauthor

    Mr. Alexis Conte, France, Euroconsult

    Coauthor

    Ms. Badia Belkouchi, France, Euroconsult

    Coauthor

    Ms. Ameli Schwalber, Germany, concentris research management gmbh

    Coauthor

    Ms. Barbara Heißerer, Germany, concentris research management gmbh

    Year

    2018

    Abstract
    SOAR (Satellite for Orbital Aerodynamics Research) is a CubeSat mission designed to investigate the interaction between different materials and the atmospheric flow regime in very Low Earth Orbit and to demonstrate aerodynamic attitude and orbit control manoeuvres. Improving knowledge of the gas-surface interactions is important for the design of future satellites operating in lower altitude orbits and will enable the identification of materials which can minimise drag or improve aerodynamic control, a key aim of the Horizon 2020 funded DISCOVERER project. In order to achieve these objectives, SOAR features two payloads: i) a set of steerable fins which provide the ability to expose different materials or surface finishes to the oncoming flow with varying angle of incidence whilst also providing variable geometry to investigate aerostability and aerodynamic control; and ii) an Ion and Neutral Mass Spectrometer with Time-of-Flight capability which enables accurate measurement of the in-situ flow composition, density, and thermospheric wind velocity. The drag and lift experienced by the satellite in orbit can be studied and estimates of the aerodynamic coefficients calculated using precise orbit and attitude determination information and the in-situ measured atmospheric flow characteristics. This paper first presents the scientific design and operational concept of the SOAR mission, focusing on the stability and control strategy which enables the spacecraft to maintain the flow-pointing attitude required by the payloads. The methodology for recovery of the aerodynamic coefficients from the measured orbit and in-situ atmospheric data is then presented. Finally, the uncertainty of the resolved aerodynamic coefficients is estimated statistically using simulations.
    Abstract document

    IAC-18,B4,2,2,x43107.brief.pdf

    Manuscript document

    IAC-18,B4,2,2,x43107.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.