molecular spectroscopy symposium 2008 16-20 june 2008 high resolution molecular spectroscopy for...
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Molecular Spectroscopy Symposium 2008 16-20 June 2008
HIGH RESOLUTION MOLECULAR SPECTROSCOPY FOR PLANETARY EXPLORATION
John C. Pearson, Brian J. Drouin, Ken Cooper, Anders John C. Pearson, Brian J. Drouin, Ken Cooper, Anders Skalare, Mark Allen and Christopher Webster Skalare, Mark Allen and Christopher Webster
Jet Propulsion Laboratory, California Institute of Technology, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109Pasadena, CA 91109
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NASA Planetary Science GoalsNASA Planetary Science Goals
Mars Science Goals, Objectives, Investigations. and Priorities: 2006 http://mepag.jpl.nasa.gov/reports/MEPAG%20Goals_2-10-2006.pdf
– Geological History of water (18O:16O and H:D ratios)
– Identify and characterize phases containing C, H, O, N, P and S
– Carbon Cycling and 12C:13C ratios
– Identify complex organics
– Atmospheric O3, H2O2, CO, OH, CH4, SO2….
Astrobiology Road Map: 2008 http://astrobiology.arc.nasa.gov/roadmap/– Water, atmospheric gas, organics on Mars
– Origins and evolution of functional biomolecules
– How to recognize signatures of life
Solar System Exploration Road Map 2006 http://www.lpi.usra.edu/vexag/road_map_final.pdf
– Understand the original composition of solar system bodies
– Isotopic ratios yielding insight into time evolution
– Chemical and isotopic composition
– Study organics on Titan, Europa & Enceladus
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Fundamental Instrument ConsiderationsFundamental Instrument Considerations
Instruments will always be too massive
– Few Kg is an upper limit
Instruments will always be too power hungry
– Few watts is an upper limit
Instruments will always have to be launched
– Lots of test and analysis is required
Instruments will always have to survive the space environment
– More tests, analysis and non-optimal electronic components
Corollary: Instruments will always be too expensive
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Some Previous InstrumentsSome Previous Instruments
Major planetary instruments– Mass Spectrometers
Viking GCMS INMS Venus, Galileo, Cassini etc… Galileo Probe GCMS Huygens Probe GCMS
– Spectroscopy Low resolution UV and Visible (Mariner, Galileo, Cassini, …) Low resolution IR and Visible (Mariner, Galileo, Cassini,…)
Limb sounder (Comet only so far)– MIRO instrument on Rosetta has 550-600 GHz heterodyne receiver
Remote Observation– Radio Astronomy (Molecular Global Average & Line shape)
– IR Astronomy (Molecular Global Average) ISO SWAS, ODIN
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Tunable Laser Spectrometer (TLS)Tunable Laser Spectrometer (TLS)
In Situ Science:
CO2 (with 12C/13C and 16O/17O/18O ratios in CO2) evolved from solids and in atmosphere;
CH4 abundance [w/SAM pre-conc.] 3 orders of magnitude better than current estimates of 10 ppb; 12C/13C ratio in methane.
Technology:NIR laser – Nanoplus, GermanyInterband Cascade (IC) Laser
– JPL Manufactured LaserPI:
Christopher Webster-JPLMission
Part of Sample Analysis at Mars (SAM) instrument (includes GCMS and sample handling)Mars Science Lander Launch 2009
NIR Laser IC Laser
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TLS IITLS II
• Free running laser spectrometer2 sealed reference cells for calibration
• 20cm base path Herriott cell81 passes (16.8 m) on methane 2ppbv43 passes (8.6 m) on CO2 1ppmv43 passes (8.6 m) on H2O 2ppmv
• Isotope ratios CH4 and CO2
3% at 30ppmv on 13CH4
2-5% at 3ppmv on 18O/17O/13C CO2
Optical demonstration of 6 channel Herriott Cell
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TLS IIITLS III
13CH4H2O CO2 OC18O
13CO2
OC170
CH4
Test data from TLS: Both spectra are from Laboratory AirSystem records direct detector DC, 2f low gain, and 2f high gainBoth reference and science channels are recorded3.8 Kg, 42 Watts worst case power consumption
First and so far only high resolution in situ spectrometer
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Earth Observing InstrumentsEarth Observing Instruments
Some Moderate to high resolution Spectrometers
– Atmospheric Trace Molecule Spectroscopic Experiment (ATMOS)
– Cryogenic Infrared Spectrometer and Telescope for the Atmosphere (CRISTA)
– Atmospheric Infrared Sounder (AIRS)
– Tropospheric Emission Spectrometer (TES)
– Atmospheric Chemistry Experiment (ACE)
Microwave Instruments
– UARS Microwave Limb Sounder
– EOS Microwave Limb Sounder
– ODIN in Limb Sounder Mode
Long History of increasingly sophisticated spectroscopic instruments
– Technology has not yet made it to the other planets
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Sensitivity Considerations for Active InstrumentsSensitivity Considerations for Active Instruments
Long Ago Townes and Geschwind derived an upper limit for spectroscopic detection with an active instrument
Where Prx is the received power and is the post detection bandwidth
Real systems rarely achieve this source noise dominated limit
The signal to noise ratio of real Heterodyne detectors is
The signal to noise ratio of a direct detector is
Where is the quantum efficiency, f is the detected bandwidth, is the frequency and NEP is the intrinsic noise equivalent power. If hv>kT first term dominates otherwise the second dominates
Note that NEP is likely to be strongly affected by the total input power level
rxvPkTP 22min
rxsys
rxrx
vPkT
P
P
PSNR
22min
vNEPvhvPfvkTvPkT
P
P
PSNR
rxrx
rxrx
22min )(22
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Radar SpectroscopyRadar Spectroscopy
Requires a thin atmosphere or exosphere
Transmit signal in at least 3 closely spaced tones
Detect in as narrow bandwidth as possible (1/pulse time)
Ratio to detect absorption
Noise is source noise + speckle noise (proportional to surface relief and spacecraft velocity)
Strong lines can be detected at a few ppm in a column of 1016 over relatively smooth surfaces
2 2
3 44t
r
PGP
R
Note: It is a relatively trivial addition toobtain brightness temperature (shown), to have a passive spectrometer or to do ranging
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““Microwave” SpectrometersMicrowave” Spectrometers
All polar molecules have rotational band making millimeter/submillimeter systems ideal for detecting a wide range of molecules
This potential for microwave spectrometers as gas analyzers was recognized long ago
– Requires low power consumption All solid state is necessary
– Requires wide electronic tuning range Synthesized or calibrated free running
– Requires high sensitivity without cryogenics Ambient temperature detection
Microwave electronics can also survive a wide range of environments (20K-380K)
– Ideal for in situ studies with access to surface or atmosphere
– Can be made work with >10% tuning range to >1 THz
Limit of detection in ideal cases ~1 part per trillion in the volume
Spectrum of simulated Titan atmosphere5% CH4 / 95% N2 in cold DC discharge
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Limb SoundersLimb Sounders
The MIRO instrument on Rosetta is the first planetary limb sounder
– H2O, CH3OH, NH3 in a comet encounter (in route now)
Other limb sounders have been proposed– Marvel for Mars (540-600 GHz)
– Submillimeter Line Spectrometer (SLS) for Venus (540-620 GHz)
– Titan/Jupiter concepts under development Several bands including 1200 GHz on Titan for CH4 & NH3
– Bandwidth, Mass, Power and $$$ are the big challenges
Potentially useful with very tenuous atmospheres– Better in case where more gas is present
Can also be done at shorter wavelengths or with occultation
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Other ChallengesOther Challenges
Several key spectroscopic challenges exist
– Remote observation of solid material content Preferable imaging with no moving parts Parts per million sensitivity is needed
– Improved resolution IR-UV spectrometers Preferably imaging with no moving parts Small and low power
– Theoretical limited sensitivity
Spectroscopic instruments all require laboratory measurements
– Supporting the development, calibration and data reduction for these and similar instruments is a major opportunity for spectroscopists
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AcknowledgementAcknowledgement
This work was performed at the Jet Propulsion Laboratory, California Institute of Technology, under contract with the National Aeronautics and Space Administration