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NETwork studies of MARS climate and interior A.V.Rodin, V.M.Linkin, A.N.Lipatov, V.N.Zharkov, T.V.Gudkova, R.O.Kuzmin.

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Presentation on theme: "NETwork studies of MARS climate and interior A.V.Rodin, V.M.Linkin, A.N.Lipatov, V.N.Zharkov, T.V.Gudkova, R.O.Kuzmin."— Presentation transcript:

1 NETwork studies of MARS climate and interior A.V.Rodin, V.M.Linkin, A.N.Lipatov, V.N.Zharkov, T.V.Gudkova, R.O.Kuzmin

2 Scientific priorities of Mars exploration: what’s done? Climate dynamics (atmospheric temperature, water, dust, clouds) Surface and subsurface volatiles inventory Paleoclimate records in surface composition and morphology Extra rare constituents (methane)

3 Future plans NASA: Mars Science Laboratory (rover), MAVEN (atmosphere sample analysis). Soil sample return mission in a foreseeable perspective. ESA: ExoMars – rover with drilling capabilities.

4 What’s to be done by orbiters Wide-field hyperspectral monitoring (analog of VEX/VIRTIS) High resolution spectroscopy in IR and/or microwave ranges for isotopic analysis and Doppler measurements (present in NASA and ESA programs)

5 What’s to be done by landers Mars internal structure and composition - a network of seismometers Meteo network Surface thermal & electric conductivity – penetrating probes (depth 10-20 cm )

6 How many stations do we need in a network? According to Kotelnikov theorem, 4 seismic and 6 meteo stations should be placed in each latitude zone Wave 3 feature in water vapor (model) 00 180  10 20 30 40 50 60

7 Minimalistic concept: 2 “light” stations in the polar regions 2 “heavy” stations in tropics or midlatitudes

8 MEX/OMEGA 1.5  m index MGCM SHNH

9 Technical heritage: Netlander (ESA) MET-NET (IKI & FMI) microlanders

10 Lavochkin’s view on mission scenario

11 Wind Sensor Thermocouples 100 cm Soil Probe Temperature, Humidity Imager & opt. sens. Model science payload MET- Boom Descent phase instr. package P, T, Acc Surface phase instruments: Seismic sensor Pancam Wind speed sensor Pressure Atm. temperature Atm. humidity Soil temperature Soil humidity Lidar

12 Thermal & electric conductivity probe (Phoenix experience)

13 seismic measurements: high demands on sensitivity

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15 First IBU Inflatable heat shield

16 Main IBU

17 Mass Budget

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19 Thermal protection system tests

20 MetNet Flight Test Испытания ТЗП

21 2007 Inflatable heat shield tested using Volna launcher for suborbital flight

22 Resume A network mission to Mars with small stations bearing meteo package, seismic sensors and optional instruments may get a high priority for the Russian national space program. Rich technical heritage and connection with European and US groups involved in similar network missions leaves a hope that it will be implemented shortly


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