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  Scientific objectives of the seismic experiment
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Main objectives of the seismic NetLander experiment are to determine :

  • the mean value of shearing and incompressibility coefficients versus the depth, the core/mantle interface, the core state, the position and features of mantle discontinuities, and the crust thickness ;
  • the mean attenuation and its variation with depth ;
  • at a regional scale, or at least vertically to each station : crust thickness and other crustal interfaces, including markers associated to the 0°C isotherm inside pergelisol ;
  • the level and geographical distribution of seismic activity on Mars and its link with surface tectonics.

Those seismic measurements combined with high resolution imaging will moreover allow :

  • to specify geometry of tectonic structures,
  • to model deformation mechanisms,
  • to relate these mechanisms with volcanic activity,
  • to constrain the models of the planet internal dynamics and geological evolution.

Together with the geodesy experiment (moments of inertia measurement) coupled to high pressure experiments, those results are expected to lead to an average model of the mineralogical composition of the planet versus the depth, and to an average temperature model. With 3 operational landers, preliminary information would be obtained about the amount of lateral heterogeneity, particularly thanks to the surface waves focusing-defocusing.

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  The instrument
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The proposed instrument consists of :

  • two very broad band axes (V.B.B.) developed by the Institut de Physique du Globe de Paris (IPGP) in the framework of a CNES Research and Technology program ;
  • micro-sensors developed by the jet Propulsion Laboratory (JPL) ;
  • an electronic system developed by the Polytechnic School of Zurich (ETH) for experiment control and data acquisition.

The instrument benefits from the OPTIMISM experiment developed by the IPGP and the DT/INSU during the past mission Mars96.

This association will carry out a very broad band detector (VBB) (0.1mHz - 10Hz) of high performance with two measurement axes : horizontally and vertically, plus another horizontal broad band short period axe (BRB) (10mHz - 10Hz), offering then a tri-axial detection. Moreover, another sub-vertical JPL micro-sensor will provide a short period output (SP) (10mHz - 50Hz). The detection of tide signal will also be assumed by one of the VBB sensor outputs. Quasi-fullness of the seismic and gravimetric signals will thus be measured.

Seismometer data will be digitized at 20 samples per second for the two VBB components and the BRB component, and at 100 samples per second for the SP component. Those data will be stored in the lander mass memory, and will allow to calculate a filtered output at 1 sample per second of the vertical signal, and also regular measurements of the spectral amplitudes for frequencies over 1 Hz. This mass memory is able to store all signals recording during two weeks.

Vertical LP signal , continuous spectral measurements and tide signal will be regularly transmitted. Terrestrial operators will thus be able to identify temporal windows with interesting signals. High sampling rate signals VBB, BRB and SP will then be transmitted to Earth on request.

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   Prototype 1 VBB seismometer axe (to the left)

JPL micro-sensor description (to the right)

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The integration of VBB sensors and of one of JPL sensor takes place in a 18cm-diameter vacuum sphere. The seismic experiment whole mass (sensors + electronics) is 1750g.

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   Zoom (24 Ko)

VBB and JPL prototypes seismometers performances and those expected for the flight models

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  The SEISmometer-NetLander team
 

Scientific team

Principal Investigator

Philippe Lognonné

IPGP, Saint Maur

Principal Co-Investigator, SP sensor

Bruce Banerdt

JPL, USA

Principal Co-Investigator, electronics Domenico Giardini ETH, Switzerland
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Co-Investigators and responsability (shared with PIs)

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IPGP data center

Jeaninne Gagnepain-Beyneix

IPGP, Saint Maur, France

Calibration Jacques Hinderer EOPG Strasbourg, France
  Jean-Jacques Lévêque EOPG Strasbourg, France
 

Luis Rivera

EOPG Strasbourg, France

Link with geodesy Véronique Dehant ORB, Brussels, Belgium
 

Pascale Defraigne

ORB, Brussels, Belgium

Thermal correction

Paul Vauterin

ORB, Brussels, Belgium

Mechanisms determination

Anne Deschamps

University of Nice, France

Tomographic models

Jean Paul Montagner

IPG Paris, France

Meteorites detection

Jurgens Oberst

DLR Berlin, Germany

Diffraction modeling and ground tests

Michel Campillot

Grenoble Observatory, France

Link with theoretical groups

Doris Breuer

Univ. Münster, Germany

Selection of landing sites

Antoine Mocquet

University of Nantes, France

Control of mechanical I/F

Tilman Spohn

Univ. Münster, Germany

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Technical team SEISmometer-NetLander

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Project Manager SEISmometer NetLander

Patrick Schibler

IPGP, Saint Maur

VBB manager

Jean François Karczewski

IPGP, Saint Maur

System Engineer

David Mimoun

CNES/INSU, Saint Maur

Engineer, software & Electronics

Alain Desautez

IPGP, Saint Maur

Engineer, GSE, software

Taoufik Gabsi

IPGP, Saint Maur

Engineer, Electronics

André Anglade

IPGP, Saint Maur

Engineer Assistant, CAD, VBB, mechanisms

Nicolas Striebig

IPGP, Saint Maur

Engineer Assistant, Electronics

Henri Vacherat

CNES/INSU, Saint Maur

Technician, Integration, tests

Olivier Pot

IPGP, Saint Maur