EGU 2020 6566 2022 Lander Radioscience La Ra

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EGU 2020 -6566 2022 Lander Radioscience (La. Ra) in Exo. Mars 2020 to obtain

EGU 2020 -6566 2022 Lander Radioscience (La. Ra) in Exo. Mars 2020 to obtain the rotation and orientation of Mars. Véronique Dehant 1, Rose-Marie Baland 1, Sébastien Le Maistre 1, Ozgur Karatekin 1, Marie-Julie Péters 1, Attilio Rivoldini 1, Ertan Ümit 1, Tim Van Hoolst 1, Marie Yseboodt 1, William M Folkner 2 and Alexander Kosov 3 (1) Royal Observatory of Belgium, Brussels, Belgium, (2) Jet Propulsion Laboratory, United States, (3) IKI Space Research Institute of the Russian Academy of Sciences, Moscow, Russia

EGU 2020 -6566 Past Present? Objectives of La. Ra: Rotation and interior of Mars

EGU 2020 -6566 Past Present? Objectives of La. Ra: Rotation and interior of Mars and habitability Present? or future? liquid core X-band radiolink Hz 0] G 9 1. 7 , 5 4 n [7. 1 Uplink i Coherent maser D GHz ] 0 5 4. 8 , transponder 8. 400 [ n i k n i l own

EGU 2020 -6566 1. La. Ra development status report • PDR 2017, CDR 2018

EGU 2020 -6566 1. La. Ra development status report • PDR 2017, CDR 2018 • Compatibility tests at ESOC 2018: Excellent ADEV performance! • Delivery 2019 targeted value obtained value

EGU 2020 -6566 2. Ground stations • Baseline ground stations to close link with

EGU 2020 -6566 2. Ground stations • Baseline ground stations to close link with La. Ra (5 Watt out) is NASA DSN – 70 m antennas • Operational needs: twice a week for one hour

EGU 2020 -6566 3. Mission geometry SEP = Sun-Earth. Probe angle (elongation) Time (years)

EGU 2020 -6566 3. Mission geometry SEP = Sun-Earth. Probe angle (elongation) Time (years) Pink boxes: Small Sun-Earth-Probe angle (= elongation), meaning a larger noise on the data Grey boxes: Small Earth declination

EGU 2020 -6566 4. Expectations • La. Ra is a Belgian instrument selected on

EGU 2020 -6566 4. Expectations • La. Ra is a Belgian instrument selected on the Exo. Mars surface platform of Roscosmos/ESA mission. • La. Ra will provide information on interior of Mars, its evolution, as well as CO 2 sublimation/ condensation process between the atmosphere and the ice caps. • synergies between In. Sight / RISE and La. Ra are very valuable; • synergies with all atmospheric data are very valuable too.

EGU 2020 -6566 5. Expected results (1) Mars Orientation Parameters (MOP) Model Max. MOP

EGU 2020 -6566 5. Expected results (1) Mars Orientation Parameters (MOP) Model Max. MOP amplitude Max. change Geophysical in the lander Properties position Nutation in obliquity ( ) Nutation in longitude ( ) Liquid Core effect Trigonometric series (annual, ½, 1/3, …) Liquid core amplification in the nutations 10 m 30 m 12 m 0. 7 m on d , 0. 4 m on d 0. 4 m Precession Rate (uncertainty of 2 mas/y) Length-of-day (LOD) variations Polar motion (PM) Rate 0. 8 m Trigonometric series (annual, 1/2, 1/3, …) Trigonometric series 12 m 1. 2 m Cf (Mars core moment of inertia) Core state, core size, core density C (Mars moment of inertia) Atmosphere and ice caps dynamics

EGU 2020 -6566 5. Expected results (2): Nutation estimates Estimated uncertainties on the amplitudes

EGU 2020 -6566 5. Expected results (2): Nutation estimates Estimated uncertainties on the amplitudes of the semi-annual prograde nutation and ter-annual retrograde nutation as a function of the mission duration. The uncertainties are superimposed with the expected effect that a planet with a liquid core would have on those nutations (grey boxes). These predicted uncertainties will be further reduced when combining La. Ra’s data with In. Sight-RISE data.

EGU 2020 -6566 5. Expected results (3): Nutation estimates Measurement of the nutation parameters

EGU 2020 -6566 5. Expected results (3): Nutation estimates Measurement of the nutation parameters (in particular the ter-annual retrograde amplitude) will allow us to constrain the size of the Martian core as well as its moment of inertia and flattening.

EGU 2020 -6566 6. Determination of the position of the lander La. Ra alone

EGU 2020 -6566 6. Determination of the position of the lander La. Ra alone can be used to estimate the coordinates (including Z) of the Exo. Mars 2020 Surface Platform (SP) at the level of tens of meters after only two days of DTE Doppler tracking operations.

EGU 2020 -6566 Thank you for your interest!!!! Acknowledgements This work was financially supported

EGU 2020 -6566 Thank you for your interest!!!! Acknowledgements This work was financially supported by the Belgian PRODEX program managed by the European Space Agency in collaboration with the Belgian Federal Science Policy Office.