ESA and the Moon Bernard H. FOING Chief Scientist & Senior Research Coordinator ESA RSSD/ ESTEC
http://sci.esa.int/smart-1/ www.esa.int BHF 2008 Solar System
Cassini- C Huygens O Rosetta 04 S M I C ExoMars V Smart 1 Mars Express I S
Solar I Chang’E1 Orbiter O Chandrayaan-1 > 2015 N Venus Express 05 BepiColombo 2013 BHF 2008 SMART-1 latest results for future lunar exploration Bernard H. FOING & SMART-1 team
http://sci.esa.int/smart-1/ www.esa.int BHF 2008 SMART-1 Mission (http://sci.esa.int/smart-1/)
• ESA SMART Programme: Small Missions for Advanced Research in Technology – Spacecraft & payload technology demonstration for future cornerstone missions – Management: faster, smarter, better (& harder) – Early opportunity for science
SMART-1 Solar Electric Propulsion to the Moon – Test for Bepi Colombo/Solar Orbiter – Mission approved and payload selected 99 – 19 kg payload (delivered August 02) – 370 kg spacecraft – launched Ariane 5 on 27 Sept 03, Kourou – 110 M Eu including launch
BHF 2008 Europe to the Moon: spacecraft, launch, operations (ESA+ industry) Instruments PIs + TIs from 5 countries Co-Is from 13 ESA + 6 non European countries
BHF 2008 Solar Electric Primary Propulsion: 7 g thrust, 60 liters Xenon to the Moon
BHF 2008 SMART-1: With Sun power to the Moon on 60 liters of fuel
De la Terre à la Lune (Jules Verne) BHF 2008 Solar Electric Propulsion to the Moon – Launched 27 Sept 2003 as Auxiliary passenger on Ariane 5 into Geostationary Transfer Orbit – Spiral out cruise (13.5 month): – lunar capture 15 November 2004, spiral down – arrival 15 March 05 science (450 -2900 km): commissioned spacecraft/instruments at Moon, nominal science mission March-July 05 – reboosting 2 aug-15 Sept 05 to increase orbit lifetime for extension phase until 3 Sept 2006
BHF 2008 Moon Phase & Mission Extension
MISSION EXTENSION
Apolune
Perilune
Moon Radius
BHF 2008 Smart-1 Impact
LEARNING TO LAND: SMART-1 IMPACT ON THE MOON
Courtesy of Mark R Rosiek USGS Astrogeology Team, Planetary Geomatics Group and Dr Anthony C.Cook, School of Computer Science and IT,University of Nottingham,
BHF 2008 Our last Moon travelling shot
BHF 2008 Technical achievements: Innovative Technologies on Smart-1
Sun SMART-1 light
Reflected Sun light
KA-band antenna Triple junction solar cells Multicolor microcamera
Laser Link
Communication X-Ray Spectrometer On-board computer
Lithium ion batteries Infrared Spectrometer OBAN Platform Autonomy Technologies Miniaturisation
BHF 2008 What shapes rocky planets?
Polar regions cratering Bombard ment chronolog y
SMART-1 impact Tectonic wrinkles volcanism Prospector H map BHF 2008 SMART-1 view of Hadley Rille (giant lava tube) near Apollo 15 landing site
100 km field
BHF 2008 Coupling between impacts and volcanism - Humorum: Multiringed impact basin - Procellarum: Irregular basin - Tectonics of mascon loading
Peters et al 2007, 2008
BHF 2008 SMART-1
Clementine
From imagination to reality Jules Verne crater: Volcanism in
South Pole-Aitken Basin BHF 2008 BHF 2008 SMART-1 results and feed forward (poster session) Despan et al High resolution maps with AMIE /SMART-1
Peters S. et al Future Robotic study of Lunar Basins
Borst,Bexkens, Foing Geological and Geochemical study of SPA Basin
BHF 2008 50 km
SMART-1 Mosaic of North polar region
Mapping support to future lunar exploration: landers, rovers and
North Pole human bases BHF 2008 Hermite North Pole
Rozhdestvenskiy 3D View Reconstruction
Plaskett
BHF 2008 Earth Lunar South Pole
20 km
Shackleton crater Shoemaker deGerlache
Amundsen crater (84.5º S, 82.8º E) ZOOM Faustini crater
BHF 2008 10 km
Amundsen crater
BHF 2008 Shackleton crater
BHF 2008 Shackleton rim
SMART-1 Peak of Light
BHF 2008 SMART-1 Peak of Light
BHF 2008 BHF 2008 • ESA contribution to Chang’E1 – ESA support to mission – Ground station, control and data reception – SRE, LEX, OPS
• ESA contribution to Chandrayaan-1 – SIR2, C1XS, SARA instruments – lessons learned from SMART-1 – ESA support to mission –SRE
BHF 2008 LES3 study • Lander station element – Technology survival, operations – Geophysical network – Life sciences/environment • Rover element – Close range mobility 50 m: nanorover – Regional mobility 1-10 km: Exomoon rover – Vertical mobility (penetrating sensors, moles, drill)
• Lunar Robotic Challenge • Communication/navigation/survey infrastructure: – Small orbiter with stereo camera and data relay – Exchange/support other international orbiters/landers
BHF 2008 Lunar Polar Lander Concept
1) Precise Landing on the Moon 2) Preparation of future exploration & sample fetcher 3) Geochemical study of polar regions 4) Ice Search/ characterisation
¾ Lander station element ¾ Rover element ¾ Robotic challenge ¾ Orbiter and relay infrastructures
¾ Opportunities for Students, education, outreach, cultural, artistic experiments
¾ Part of global robotic village with Chang-E2, Selene 2,
and supporting International Lunar Network… BHF 2008 Conceptual design for lunar regional ExoMoon rover inherited from ExoMars
BHF 2008 Instruments for Moon landers (100-180 kg): • ELP European Lunar Geophysics package: 15-20 kg – Seismometer, Geodesy and laser , Heat flux, Magnetometer (coordinated with Intl Lunar Network) • Lander instruments: 10 kg – Cameras: Descent, Pan Cam, Stereo, SRC – Local sample analysis (GCMS), permittivity • Life science/environment experiments : 7 kg – Radiation/ environment/planetary protection studies – Melissa bacteria precursor, plants on the Moon • Close proximity Rover: 5 kg – Neutron spectrometer, APX , Close up camera – Electromagnetic sounder, Ground penetrating radar • ExoMoon Regional rover : 120 kg – Navigation and hazards avoidance, inspection cam, – Robotic arm (PAW like), drill and mole , Active seismic, – LIBS, Fluorescence, Thermal IR fluorescence – Dust lifting measurement device, QCM or cube piezo • Lunar robotic challenge to access ice in dark: 15 kg . nanorover, harpoon, impactor, … BHF 2008 Tethered small rovers 4-10 kg
BHF 2008 Rock Corer Hong Kong Polytechniq Mössbauer Spectrometer Microscope University of Switzerland, Stereo Mainz, Germany MPEA Germany Camera MSSL, UK Stereo Camera
X-Ray Spectrometer Sampling University of Mole Leicester, UK DLR, Germany
BHF 2008 PAW Courtesy M. Sims Leicester U. NEXT call for ideas: lunar • Lunar Robotic Sample Return • Materially Self-sufficient Production for a Lunar Colony • Integrated Lunar Demonstration Mission with Landing Science Package (Moon Farside Explorer) • Lunar Sample Return • A European Lunar Scientific and Robotic Lander Mission • Lunar Dust Observatory • Lunar Sample Return Entry and Aerocapture Demonstration Mission (LEAD) • Lunar Sample Return Missions • Direct Lunar Sample Return Mission • Lunar Exploration Lander • Surface Navigation Services • Active Seismic Survey for Planetary Drilling • Teleoperated Lunar Drilling – Exploiting Synergies with the Oil and Gas Exploration Sector • ISRU Demonstration Facility on Lunar Surface • MoonSailor • Lunar Infrastructure For Exploration - Astronomy & Space Science Mission • MoonTwin • Exploration of Lunar Craters at the Moon's South Pole • Landing of an Astrobiological Habitat at the Moon's South Pole • Landing of an Astrobiological Habitat and a Micro-Rover at the Moon's South Pople • Lunar Sample Return
BHF 2008 Robotic precursors, Technology developments Defining the path for human return to the Moon
Carpenter et al Moon-NEXT mission
Visentin, et al ESA’s Lunar Robotics Challenge
Walker R. et al European Student Moon Orbiter
Hovland S. ESA preparation for Human Exploration
Boche-Sauvan et al Constraints on Pre-Design of Minimal Human Lunar Outpost
Hufenbach et al NASA-ESA comparative architecture assessment
Mongrard et al European architecture for Lunar Exploration
Wills, Foing Astrobiology and exposure experiments from the Lunar surface
BHF 2008 BHF 2008 European Aurora Programme Roadmap (updated from 2001)
NEXT Techno Demo
2013 2015 2020 2025 2035
Mars Sample Return
BHF 2008