Title: ESA technology development activities for fundamental physics space missions
1ESA technology development activities for
fundamentalphysics space missions
- B. Leone, E. Murphy, E. Armandillo
- Optoelectronics Section
- ESA-ESTEC
- European Space Research and Technology Centre
- European Space Agency
- Noordwijk, The Netherlands
2Outline
- Presentation of the Optoelectronics Section
- Fundamental Physics Missions at ESA
- Cosmic Vision
- Technology Needs for Future Fundamental Physics
Missions - Technology Development Strategy
- Earth Observation and Planetology
- Current and Planned Activities
- Conclusions
3Optoelectronics Section
- Head Errico Armandillo
- Team of experts
- Detectors
- X-rays
- UV, VIS, IR
- FIR, THz, (sub)mm-wave
- Photonic devices
- Fibres and sensors
- Optical telecommunication
- Lasers
- Lidar
- Distance metrology
- Frequency standards
- Laser-cooled atom interferometry
- Laser damage (laboratory)
4Terms of Reference
- Optoelectronic device technologies and
applications - Laser technology and components
- Photonic integrated optics
- Non-linear optics
- Superconductor technology
- Far-IR heterodyne instrument design and
verification gt 1 THz - Detector technology and radiometry for the X-ray,
UV, IR and Far-IR (incoherent and heterodyne) gt 1
THz
5Our Role within ESA
- Directorate of Technical and Quality Management
- Support Directorate within a matrix organisation
- Customers
- Science
- Human Spaceflight, Microgravity and Exploration
- Earth Observation
- Applications
- Telecommunications
- Navigation
- Initiate technology development activities in
support of programmes and to enable future
missions - Provide technical expertise to projects
6Technology RD
- Initiate and follow up technology development
activities up to Technology Readiness Level 5/6 - TRL1 - Basic principles observed and reported
- TRL2 - Technology concept and/or application
formulated - TRL3 - Analytical and experimental critical
function and/or characteristic proof-of-concept - TRL4 - Component and/or breadboard validation in
laboratory environment - TRL5 - Component and/or breadboard validation in
relevant environment - TRL6 - System/subsystem model or prototype
demonstration in a relevant environment (ground
or space) - TRL7 - System prototype demonstration in a space
environment - TRL8 - Actual system completed and "flight
qualified" through test and demonstration - (ground or space)
- TRL9 - Actual system "flight proven" through
successful mission operations
7ESA Technology Landscape
8Qualification and Reliability
- Laser laboratory facility
- Laser diode reliability test envisaged
- Low to high power laser diode multimode
emitter/bars/stacks - CW pumping (1-30 Watts) at 808, 9xx nm
- QCW pumping ( 100 Watts peak power)
- Qualification and reliability aspects
- Optical components
- Laser diodes
9Outline
- Presentation of the Optoelectronics Section
- Fundamental Physics Missions at ESA
- Cosmic Vision
- Technology Needs for Future Fundamental Physics
Missions - Technology Development Strategy
- Earth Observation and Planetology
- Current and Planned Activities
- Conclusions
10Fundamental Physics Missions at ESA
- Science
- LISA (Laser Interferometer Space Antenna)
- Search for gravitational waves
- 50 NASA
- Technology RD not shared
- LISA Pathfinder (LTP)
- Technology demonstrator mission
- LISA precursor mission
- Cosmic Vision
- Human Spaceflight, Microgravity and Exploration
- ACES (Atomic Clock Ensemble in Space) onboard the
ISS - Main goal technology demonstrator
- Test a cold atom clock in space
- Test a hydrogen maser in space
- Time and frequency comparison with ground clocks
- Three fundamental physics tests
- Gravitational red shift increased accuracy
- Search for fine structure constant drift
- Search for Lorentz transformation violations
11Outline
- Presentation of the Optoelectronics Section
- Fundamental Physics Missions at ESA
- Cosmic Vision
- Technology Needs for Future Fundamental Physics
Missions - Technology Development Strategy
- Earth Observation and Planetology
- Current and Planned Activities
- Conclusions
12Cosmic Vision 2015-2025
1
- 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?
1 Cosmic Vision Brochure BR247
http//www.esa.int/esapub/br/br247/br247.pdf
13Cosmic Vision 2015-2025
- Explore the limits of contemporary physics
- Use stable and weightless environment of space to
search for tiny deviations from the standard
model of fundamental interactions - The gravitational wave Universe
- Make a key step toward detecting the
gravitational radiation background generated at
the Big Bang - LISA follow-up mission
- Matter under extreme conditions
- Probe gravity theory in the very strong field
environment of black holes and other compact
objects, and the state of matter at supra-nuclear
energies in neutron stars - X-ray and gamma ray astronomy
14Fundamental Physics Explorer Programme
- Do all things fall at the same rate?
- Cold-Atom interferometer
- Do all clocks tick at the same rate?
- Optical clocks
- Does Newtons law of gravity hold at very small
distances? - Take advantage of the drag-free environment
- Does Einsteins theory of gravity hold at very
large distances? - Pioneer anomaly potential for optical clocks
- Do space and time have structure?
- Fundamental constants
- Cold-atom technology and/or ultra-stable clocks
- Does God play dice?
- BEC, atom laser, atom interferometer
- Can we find new fundamental particles from space?
- Cosmic-ray particle detection
15Outline
- Presentation of the Optoelectronics Section
- Fundamental Physics Missions at ESA
- Cosmic Vision
- Technology Needs for Future Fundamental Physics
Missions - Technology Development Strategy
- Earth Observation and Planetology
- Current and Planned Activities
- Conclusions
16Technology Needs for FPEP
17Ultra-High Accuracy Metrology
- Tests fundamental physics theories require
ultra-high accuracy metrology of - Distance
- Accelerations
- Rotations
- Time
- Focus on cold-atom technology
- stabilized lasers to cool and manipulate atoms
- atom interferometry to measure accelerations,
rotations - (optical) atomic clocks to measure time and
distance - Miniaturization and space qualification
- Micro optics, atom chips
- Reliability
18Outline
- Presentation of the Optoelectronics Section
- Fundamental Physics Missions at ESA
- Cosmic Vision
- Technology Needs for Future Fundamental Physics
Missions - Technology Development Strategy
- Earth Observation and Planetology
- Current and Planned Activities
- Conclusions
19A Compelling Strategy
- Given
- One potential fundamental physics mission
- Highly competitive, low funding environment
- Cold-atom technology will benefit from space
environment - Cold-atom technology will benefit fundamental
physics - Large effort needed to bring cold-atom technology
in space - Need to propose cold-atom technology as generic
not limited to fundamental physics (navigation,
gravimetry) - Alternatively, find more applications to
fundamental physics measurements - Seek objective commonalities with other customers
- For example Gravimetry
- Earth Observation
- Planetology
20Outline
- Presentation of the Optoelectronics Section
- Fundamental Physics Missions at ESA
- Cosmic Vision
- Technology Needs for Future Fundamental Physics
Missions - Technology Development Strategy
- Earth Observation and Planetology
- Current and Planned Activities
- Conclusions
21Gravimetry
- Studies
- EO Enabling Observation Techniques for Future
Solid Earth Missions - Optoelectronics Section Gravity Gradient Sensor
Technology for Planetary Missions - Results
- Sensitive gravimeters using very precise atomic
clock - Atom Interferometry gravity gradiometry
- Development of Optical Clocks to measure
variations of fundamental constants
1, 2
3
1 Enabling Observation Techniques for Future
Solid Earth Missions, Science Objectives for
Future Geopotential Field Mission,
SOLIDEARTH-TN-TUM-001, Issue 6, 1 Nov. 2003. 2
Enabling Observation Techniques for Future Solid
Earth Missions, Final Report, SolidEarth-TN-ASG-0
09, Issue 1, 6 May 2004. 3 Gravity Gradient
Senser Technology for future planetary missions,
Final Report, ESA ITT A0/1-3829/01/NL/ND, 13 July
2005.
22Earth Gravity Missions
- Using satellites to map global gravity field
- Measure geopotential second order derivatives
- Spherical harmonic expansion
- Geoid (equipotential)
- Gravity field
- Anomalies
- Precision (mm, mGal)
- Spatial resolution
- Temporal resolution
- Time span
23Applications
- Use satellite and ground data modelling
- Solid Earth
- Geophysics
- Geodesy
- Hydrology
- Oceanography
- Ice sheets
- Glaciers
- Sea level
- Atmosphere
- Lumped sum
- Aliasing
24Types of Missions
- High Earth orbit (HEO) satellite
- Passive laser reflector (LAGEOS)
- Laser tracking from reference ground stations
- Non-gravitational forces removed by design
modelling - High-Low Satellite-to-satellite tracking (SST)
- LEO satellite tracked by GPS type constellation
(CHAMP) - Non-gravitational forces measured by
accelerometers - Low-Low SST
- Inter-satellite ranging (GRACE)
- Combined with GPS tracking
- Non-gravitational forces measured by
accelerometers - Satellite gravity gradiometry (SGG)
- Gravity field accelerations measured by
accelerometers (GOCE) - Non-gravitational forces measured by (same)
accelerometers
25HEO mission
- Use high orbit as natural filter (low harmonics)
- GPS tracking
- Accelerometers
- High precision clock (10-16)
- Advantages
- Innovative
- Earth sciences
- Time keeping
- Fundamental physics
- Telecommunications
- Drawbacks (as compared to LAGEOS)
- Mission life time
26GOCE
- GOCE Gravity field and steady state Ocean
Circulation Explorer - Launch date 2006
- Altitude 250 km
- Orbit sun synchronous
- Main payload three-axis gradiometers
- Observables diagonal gravity gradient tensor
components, Txx, Tyy, Tzz - Predicted accuracy 100 to 6 mE/vHz
- Measurement band 100 to 5 mHz
27Future Needs
- ESA funded Earth Sciences study Enabling
Observation Techniques for Future Solid Earth
Missions by EADS Astrium - Low-low SST
- Satellite Gravity Gradiometry (SGG)
- Observables diagonal gravity gradient tensor
components, Txx, Tyy, Tzz - Required accuracy down to 0.1 mE/vHz
- Measurement band 100 to 0.1 mHz
- (Pointing rate knowledge 410-11 rad s-1/vHz)
- Will current three-axis gradiometer technology be
able to meet these requirements? - Can atom interferometry do it better?
28Planets and Moons
- ESA funded GSP study Gravity Gradient Sensor
Technology for Future Planetary Missions by
University of Twente
29Future Needs
- Volume and mass constraints
- Size TBD (assumed 10 cm)
- Weight 3 kg
- Available data line of sight
- Required accuracy 1 mE/vHz
- Airplane gradiometers
- (Earth, Mars, Titan)
- Technology review
- Superconducting devices
- MEMS
- Atom interferometry
30AI Gradiometer
- Gravity gradiometer Proof-of-Concept (Kasevich et
al.)
31Planetary Gradiometer
- Back of the envelope concept
- Assuming laser and optics miniaturisation
- Vacuum chamber size 10 cm
- Atom cloud size 5 mm
- Atomic species Cs or Rb
- Baseline 1 m
- Weight few kg?
- Could achieve 1 mE/vHz
- 1 m baseline 10-13g/vHz
- Interrogation time 10 s
Vacuum chamber with the atom cloud
g1
Gravity gradient (g1-g2)/L
1m
control electronics
g2
Laser
Optical fibers
32Outline
- Presentation of the Optoelectronics Section
- Fundamental Physics Missions at ESA
- Cosmic Vision
- Technology Needs for Future Fundamental Physics
Missions - Technology Development Strategy
- Earth Observation and Planetology
- Current and Planned Activities
- Conclusions
33What is needed
- Atom Optics
- Space qualified stable Source of Cold Atoms
- Compact laser sources for cold atom production
- To cool down atoms and control atomic beams
- Ultra-stable Raman Lasers
- For coherent matter wave splitting
- Optical frequency synthesizer
- Space qualifiable femtosecond comb
- Realisation of a feasible Optical Frequency
standard/s for space - Select most suitable option from the choices
available - Realise a completely optical atomic clock
- Design and verification
34Ongoing Activities
- Atom Optics
- Laser-cooled Atom Sensor for Ultra-High-Accuracy
Gravitational Acceleration and Rotation
Measurements - Optical Atomic Clocks
- Required linewidth narrower than for optically
pumped microwave atomic clocks - Ultra-narrow linewidth probe lasers 1 Hz
- Laser-pumped Rubidium gas cell clock
(780nm/795nm) - Solutions implemented _at_ 780nm
- External cavity diode laser (ECDL) 100s kHz
- Fabry-Perot (FP) 4-6 MHz
- Laser-pumped Caesium bean clock (852nm/894nm)
- New activity (894nm) in support of
navigation/GALILEO - New activity (894nm) ultra-narrow linewidth for a
more generic application
35Planned Activities
- Optical Frequency Synthesizer activities
- Optical Frequency Comb Critical Elements
Pre-Development - Synthesis of optical frequencies and
identification of critical issues for space
qualification - Use for future fundamental physics experiments in
space - Space Compatibility Aspects of a Fibre-Based
Frequency Comb
36Needed Measurement and Verification
- Narrow band diode laser measurements
- To support the ongoing DFB/FP activities
- To initiate new activities aimed at ultra-narrow
linewidth development - Establish consistent traceable standards in
Europe - Sources of error in linewidth determination
- Heterodyne vs homodyne
- Noise sources
- Line shape dependencies
- Diode laser measurement laboratory
- Comparison with other laboratory
37Possible Future Activities
- Laser frequencies for Optical Atomic Clocks
Some possibilities - Single ion
- Hg 282 nm
- In 237 nm
- 171Yb (Octopole) 467 nm
- 171Yb (Quadrupole) 435.5 nm
- 88Sr 674 nm
- Cold atom
- Strontium (Sr) 698 nm
- Ytterbium (Yb) 578 nm
- Calcium (Ca) 657 nm
- Calcium (Ca) 457.5 nm
- Silver (Ag) 661.2 nm
38Outline
- Presentation of the Optoelectronics Section
- Fundamental Physics Missions at ESA
- Cosmic Vision
- Technology Needs for Future Fundamental Physics
Missions - Technology Development Strategy
- Earth Observation and Planetology
- Current and Planned Activities
- Conclusions
39Conclusions
- Ongoing/planned work
- Optical Atomic Clocks
- Cold atom source for atom interferometry in space
- Still a lot to be done
- Difficult to secure funding when no clear mission
is on the horizon - Adopt strategy of developing generic
technologies - Time keeping
- Gravimetry for Earth and planets
- Navigation
- etc
- Comments and suggestions from experts most welcome
40