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09.12.2014. Turin. ALTEC. DESCENT MODULE AND SURFACE PLATFORM ExoMars Science Working Team 09-12-2014.

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Presentation on theme: "09.12.2014. Turin. ALTEC. DESCENT MODULE AND SURFACE PLATFORM ExoMars Science Working Team 09-12-2014."— Presentation transcript:

1 09.12.2014. Turin. ALTEC. DESCENT MODULE AND SURFACE PLATFORM ExoMars Science Working Team 09-12-2014

2 09.12.2014. Turin. ALTEC. Landing Module: LM includes the following main elements: – platform structure; – thermal honeycombs (THC) with mounted house-keeping systems and elements of SEC; – MarsRover assembly; – propulsion system; – landing legs; – solar array panels; – TCS elements;

3 09.12.2014. Turin. ALTEC.

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6 DM mass budget.

7 09.12.2014. Turin. ALTEC. DM mass budget.

8 09.12.2014. Turin. ALTEC. Surface Platform Science Priorities: Priority 1 Context imaging. Long term climate monitoring and atmospheric investigations. Priority 2 Studies of subsurface water distribution at the landing site. Atmosphere-surface volatile exchange. Monitoring of radiation environment at the landing site. Study of Internal Mars structure (geophysics). Priority 3 Surface soil sampling at the landing site and sample analysis (also in Rover) Search for traces of organics at the landing site (also in Rover).

9 09.12.2014. Turin. ALTEC. InstrumentDescriptionMass, kg TSPP Set of cameras to characterise environment 3.4 BIP Interface and memory unit 3.0 METEO Meteorological package 3.4 FAST Fourier spectrometer to study atmosphere 3.5 ADRON-EM Active neutron spectrometer and dosimeter 5.6 M-DLS Multi-channel Diode-Laser Spectrometer for atmospheric studies 2.6 PAT-M Radio thermometer for soil temperatures (50 cm) 0.6 Dust Suite Dust particle size, impacts and atmospheric charges 1.6 SEM Two small seismometers 1.5 MGAP GS-MC for atmospheric analysis 7.0 Russian-led instruments:

10 09.12.2014. Turin. ALTEC. Announcement of Opportunity A joint Announcement of Opportunity will request: The needed European contributions to Russian-led instruments A modest European-led contribution with instrument(s)/sensor(s) (10% of payload mass)


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