Royal Astronomical Society Discussion Meeting - 12 Nov ... · PDF fileRoyal Astronomical...
Transcript of Royal Astronomical Society Discussion Meeting - 12 Nov ... · PDF fileRoyal Astronomical...
Space Science Missions Long Term Perspective from Industry Matthew Stuttard National Lead – Future Science Programmes
Royal Astronomical Society Discussion Meeting - 12 Nov 2012
Future UK Space Missions
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ESA’s Science Programme ‘Cosmic Vision’
Four big questions What are the conditions for planet formation and the emergence of life?
How does the Solar System work?
What are the fundamental physical laws of the Universe?
How did the Universe originate and what is it made of?
One little question …
p3
Science and Exploration Beyond Phase A – in the UK
2013 GAIA – mapping a billion stars with high accuracy Service module, guidance, sensors, Science Data Processing
2014 LISA Pathfinder – preparing to detect gravity waves Prime and propulsion module, optical bench, charge management
2015 Bepi Colombo – two Mercury orbiters Spacecraft composite, electric propulsion, RIU, AIT
2017 Solar Orbiter – closely observing the sun Prime, subsystem role on AOCS, many payloads
2018 MIRI – Mid-IR Instrument on JWST PI, System engineering and assurance, AIT, delivered 2012
2018 Exomars Rover Vehicle – exo-biology Prime, Comms, vision based navigation
2019 Euclid – using 2 billion galaxies to map dark matter Industry roles: competition for sub-system roles on PLM and SVM UK Science lead on VIS instrument and data processing
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GAIA: Measuring a Billion Stars
• Create 3D model of ‘milky way’
• 1000 times more accurate than exists now
• Measure direction, distance, luminosity, temperature,
gravity and composition of 1 billion stars
• Repeat up to 80 times
• A European technological marvel
• could not be built in US
• UK industry and academia (E2V, MSSL, SSTL/SIRA)
producing key focal plane and instrument technology
(106 CCDs)
• Astrium UK
• Electrical Systems lead: achieving the highest
pointing accuracy ever in Europe
• Payload Data Handling systems (VPU)
• Propulsion, antenna, spacecraft functional
validation
Onboard time correlated to UTC to less than 1S from L2
Data volume 60 Tb in 5 years
Data down-link rate 10Mbit/S
On-board processing 13000 MIPs
• Pointing Stability 10arc Seconds (≈70 picometres at the CCD)
Star density capability up to 750,000 stars per square degree Measures 100 000 stars per second
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GAIA
Avionics Model Test Bench
Chemical Propulsion System
Integration onto Structure
Ultra-stable SiC Optical Bench & Mirrors
Focal Plane
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Planetary Surface Exploration
Beagle 2 established a UK leadership role in
Europe
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Exomars Rover:
To find evidence for
past or present life
on Mars
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Rover Vehicle – Phase B
travel 18-20km @ 100m/sol
collect samples up to 2m
deep and analyse them
Autonomous Guidance and
Navigation System
Gas gap insulationAnalytical Laboratory
Drawer (ALD)
Service Module (SVM)
Rear Bogie
Attachment
WISDOM GPR
Horns (2)
Bathtub Structure
Gas gap insulationAnalytical Laboratory
Drawer (ALD)
Service Module (SVM)
Rear Bogie
Attachment
WISDOM GPR
Horns (2)
Bathtub Structure
Phase A/B1 and before
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Juice
Juice: Jovian system tour Jupiter atmosphere & magnetosphere
Jovian moons and ring system
Europa flybys – recent active zones
Callisto flybys – early remnant
Ganymede – internal composition, habitat?
Selected as L1 mission Phase A/B1 to start Q4 2012
Instruments: UK PI and Co-I roles
Many opportunities for UK industry
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M3 Mission Candidates
Marco
Polo R
Plato
EChO
STE QUEST LOFT
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MSR Precursor Missions – 2013 Phase A
Astrium UK interest Mission analysis
Launch and transfer to Mars Return transfer to Earth
Landing system design Design of sample collection and
transfer system
PHOOTPRINT Phobos sample return
INSPIRE 3 x Mars landers
Astrium UK interest Prime and system engineering Mission analysis Carrier vehicle design Design of landers Definition of planetary protection measures
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Penetrators UK niche from MoonLITE
Multi-disciplinary community formed
Jovian Moon penetrator Ganymede and Europa studied
Key science: astrobiology, geology
Current activities focussed on proving robustness to high impact loads
Testing planned at component and system level
Cavendish Lab gas gun
Pendine sands rocket sled range
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ESA Science Missions
Industrial Development Schedule
2012 2013 2014 2015 2016 2017 2018 2019 2020 2021 2022 2023 2024
Gaia
LISA Pathfinder
Bepi Colombo
Solar Orbiter
Euclid
L2
M3
Plato L1 - JUICE
M4 M3 decision
Phase A/B1
Pre-Phase A
Phase B2/C/D
Phase A1
S1 – CHEOPS (tbc)
UK Pre-Phase A/Phase A? S2
UK Leadership of Science Missions
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The Status Quo
Space science is funded because it is valued Knowledge creation, manufacturing skills, spin-along with commercial space
UK will play major roles in leading ESA science missions to 2030 Scientifically and Industrially
IGS Recommendation 13 in principle achieved through this route
… IGS ‘restack’ is focused on growth in commercial space
World-class space science tends to advance primarily with larger missions to go further, see further, measure more precisely etc.
Conservatism on feasibility/technology Strong ‘lesson learned’ by ESA
UK cannot afford to do ‘big science’ alone
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What are the Disruptive Factors?
New Science Opportunities Can niche science still be world class?
Can UK space science be funded if it is not world class?
Unique UK technologies: instruments, platforms, space access
New opportunities in line with UK Civil Space Strategy? Bilateral collaborations
National budget ‘headroom’ necessary = squeeze existing planning
Slow pace of ESA programme CV S missions ? ESA launch CV S1 by 2017?
Can UK-led small missions be quicker?
New sources of mission funding
Direct link between Science and Growth? Knowledge exchange
Practical applications of space science
Science
Policy
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Disruptive Technologies with UK strengths
2012 2013 2014 2015 2016 2017 2018 2019 2020 2021 2022 2023 2024
Optics (ongoing)
Miniaturised sensors (ongoing)
Low Cost Platform GEO Interplanetary
Nuclear Power RHU, RTG
Lightweight deployables Solar Sail Missions Large Telescopes
Robotic and Autonomous Landed Systems
Penetrators Landers Rovers Hoppers, dirigibles, boats, climbers
Low Cost Launch Virgin Skylon
NSTP -> much else …
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Longer term mission ideas
Uranus Mission RTG could leverage science roles in a bilateral
… but not low cost
Lunar Penetrators Penetrator technology still being developed by a UK team
Asteroid sample return enthusiasm in Japan – Hayabusa was a low cost mission
science is strong in UK
mission technology is strong is UK
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Total Eclipse Mission: “The Lunar Coronagraph” Mission to fly in a near exact total eclipse
(<1.02Rs) in space for many hours to days
Forms a “Super-Giant” Space Coronagraph
with a baseline circa 376,000km! No atmospheric effects (e.g. seeing, ) and much
longer totality compared to total eclipses on Earth
Lower diffraction and lower cost alternative to
Proba-3 and HiRise formation flying missions
Offers unparalleled resolution of inner Corona
Other totality/non-totality science also possible
Novel orbit yields a “far-side” total eclipse: High energy near parabolic Earth orbit provides
initial co-rotation with Moon at its “anti-Sun” side
Non-Keplerian orbit phases maintain totality
Parking orbits provide repeat totality cycles
Astrium UK study proved feasibility without
new technology or an expensive launch: Concept now being pursued with solar scientists
at MSSL, UCL and RAL
Su
n Earth Moon
Region where
Totality zone and
Perigee co-incide
Totality
Region
Lunar Orbit
Earth Orbit
Spacecraft Orbit with
Near Parabolic Apogee
Totality Region of
interest (inc. Non-
Keplerian phase)
~3.76x105 km~3.84x10
5 km
Perigee ~760,000km
(Near parabolic apogee)
Snapshot of eclipse geometry looking onto the ecliptic plane
p21 18 May 2011
Fits the ‘growth’ agenda Space weather recognised on national risk register Real costs arise and cost savings can be demonstrated
Technical expertise in UK Tracking
Heliospheric Imager – Earth leading, stripped down Located 20 degrees off Earth-Sun line Interplanetary class of mission
Environment, propulsion and comms engineering Plasma characterisation and solar surface modelling
In-situ and remote sensors at L1 or sunwards SOHO replacement Hosted payloads using miniaturised instruments
Active Users Solar Science groups Met Office – testing operational alerts MOD
Potential Users Electrical power generators and distributors Sat operators Aviation – air traffic control, airlines Oil and Gas industry …
Directly linking science and growth:
Space Weather
p22 18 May 2011
Space Weather CDF Study
HAGRID Heliospheric Imaging for Assessment of Global and Regional Infrastructure Damage Demonstrator mission for a Space Weather early warning system
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Developing New UK Mission Concepts:
Astrium Ltd Role in Phase 0/A engineering for small science missions: feasibility is key
Complex payloads
Can requirements be met
Pointing, mag, power, gravity, accommodation, contaminations, PP …
Interplanetary
transfers -> mission analysis, GAMs
propulsion (Chemical, Electric)
communications
environment
Difficult environments: thermal, power constrained, radiation
Mission enabling technologies:
RTG, RHU, deployable structures, optics, sensors, data processing
Robotic systems, autonomous guidance systems
Reliability/surviving long cruises
Feasibility assessment
Systems engineering: Mission optimisation
Technology readiness, TRL raising and forecasting
Engineering and financial budgets
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Questions ?
www.astrium.eads.net