Lunar and Planetary Science XXXVII (2006) 1982.pdf GEP-ExoMars: a Geophysics and Environment observatory on Mars : Philippe Lognonné1, Tilman Spohn2, David Mimoun1,*, Stephan Ulamec3, Jens Biele3, the ML2SP team and the Aurora Environment team 1IPGP, St. Maur des Fossés, France 2DLR, Institute for Planetary Research, D-12489 Berlin, Germany 3DLR, Institute for Space Simulation, D-51170 Köln, Germany , *E-mail:
[email protected] Mass / average Network Instrument Heritage Description Comments kg power, W science Scientific objective: Seismic suite: 2 VBB oblique seismometers Needs soil contact, plus one Short period horizontal MEMS wind and sun SEIS Netlander (Phase B) 1,615 0,28 (Micro-Electro Mechanical System) sensor x protection and The goal of the Long-Lived Geoscience Observatory completing the trihedron. Target sensitivity < decoupling from Meteo suite: wind, temperature, pressure, partly to be replaced humidity, OD, UV spectra, dust impact. by similar Pasteur ATM Beagle-2 (flown) 0,685 0,095 x on Mars, GEP (Geophysics Package) is to initiate the Modes: low/nominal/campaign/dust devil instruments, see rates below Atmospheric electricity probe to measure setup of a permanent network of fixed stations on the electric conductivity, quasi DC electric field AEP Netlander (Phase B) 0,147 0,105 CORE (up to 300 V/m), ELF/VLF radio-electric x emissions (10 Hz to 4 kHz) planet, with the objective to operate for several years. Heat flow and physical properties package. Deployed by a mole up to 5 m deep in Martian regolith: TEM, a thermal These stations will monitor with high resolution the HP3 Beagle-2 (flown) 1,195 0,003 measurement suite (thermal conductivity, heat capacity, thermal gradient [heat flux]); DACTIL, a set of accelerometers (orientation, seismic activity and the rotation of the planet, the depth, so Tri-axial vector magnetic field sensor Champ, Astrid-2 satellites including t and attitude sensors.