A Mission to Study Water in the Local Universe Paul F. Goldsmith Jet Propulsion Laboratory California Institute of Technology Pasadena CA With thanks to Darek Lis, Imran Mehdi, Jose Sile, and Adrian Tang AU General Assembly, Focus Meeting FM 15: Water Throughout the Uni Tuesday August 4 th 2015
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A Mission to Study Water in the Local Universe Paul F. Goldsmith Jet Propulsion Laboratory California Institute of Technology Pasadena CA With thanks to.
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A Mission to Study Water in the Local Universe
Paul F. GoldsmithJet Propulsion Laboratory
California Institute of TechnologyPasadena CA
With thanks to Darek Lis, Imran Mehdi, Jose Sile, and Adrian Tang
29th IAU General Assembly, Focus Meeting FM 15: Water Throughout the UniverseTuesday August 4th 2015
The Importance of Water (Vapor)
• Important coolant of “warm” interstellar clouds having T > 100 K
• Significant reservoir of oxygen in the interstellar medium (ice and gas-phase water together)
• Valuable tracer of the motions of interstellar clouds including OUTFLOWS and COLLAPSING CORES
• Tracer of thermo-chemical history of diffuse gas via ortho-to-para ratio (OPR)
• Critical source of information on origin of Earth’s oceans from icy objects in solar system (HDO/H2O ratio)
• Critical for life on Earth and other planets
Tracing Gas Phase WaterHigh spectral resolution is essential for realizing potential of H2O as a probe of
conditions and history
Rich spectrum throughout Submillimeter and Far-Infrared – Need to make choices!
Transitions of H2O and isotopologues observed in NGC6334 with Herschel HIFI (Emprechtinger+ 2013)
Quiescent Clouds: Water frozen on dust grainsOutflows: Shocks & radiation clean grain mantles – water returned to gas phase
Water as Tracer of Dense Core Kinematics
Water: demanding excitation => tracers innermost, densest regionsC18O: easy to excite--traces overall core and its motions
Cold (8-12 K), compact (0.1 pc) dense(103-107 cm-3)Precursors to new stars; should be collapsingWhat is the velocity field in collapsing cores?
All models have ~same n(r) but vastly different v(r)
Keto,Caselli,Rawlings2015
Larson-PenstonSingular Isothermal Sphere
Unstable B-E Sphere
H2O C18O
Only the Quasi-Equilibrium Bonnor-Ebert Sphere model reproduces observations of L1544
L1544 H2O 557 GHz datafrom Herschel HIFINote velocity resolution Theoretical
Models
Water Emission in Orion
Offset (arc seconds)
Ground State (557 GHz) Emission Dominated by Broad Outflow
Herschel
Excited State – Thermal & Maser Emission
Hartogh et al. (2010) Comet C/2008 Q3 (Garradd)Deuterated Water Comet 103P/Hartley 2
111-000(para) 1113 GHz 212-101 (ortho) 1670 GHz
Water & Heavy Water in Comets: Origin of Earth’s Oceans
D/H ratio varies significantly within the solar systemEarth’s D/H ratio does NOT match that of Oort Cloud (very distant) comets
D/H ratio DID match that of first Jupiter-Family comet in which water observed
• Heterodyne spectroscopy does NOT require cold optics: translate cost savings of ambient optics to larger telescope
• Larger aperture => higher angular resolution AND higher sensitivity
• Increase data rate by using FOCAL PLANE ARRAYS and SIMULTANEOUS MULTIBAND OBSERVATIONS
• Utilize recent advances in submm receiver technology• Baseline cryocoolers rather than cryogens for receiver
cooling• Exploit Digital Signal Processing breakthroughs
Telescope Concept
• Deployable, segmented telescope to fit within shroud of low-cost launch vehicle
• Falcon 9 Heavy – direct launch to L2• 6m dia telescope (6.8m diameter possible)• 12.5” FHWM beam width @ 1 THz (λ = 300 μm) 6.5” FWHM
at λ = 158 μm• 36 hexagonal segments• Two folds (as JWST) plus secondary deployment• Overall surface accuracy ~ 10 μm rms• Various panel technologies – CFRP honeycomb, Al
honeycomb, hybrid designs• 1o C temperature gradient across deployed antenna• Orbital LEOstar-3 bus with upgraded dual star trackers for
required 1” pointing accuracy (possibly Ball HAST)• Enhanced propulsion system for orbital insertion and orbit
maintenance• Total spacecraft mass 7000 kg (probably will be less)
• Single –layer sunshield supported by 4 astromasts
• Sunshade geometry will be optimized but want to preserve ability to point relatively close to sun (especially for Solar System objects)
Solar array on opposite side of sunshield
Secondary reflector supported by tripodTelescope &
Sunshade Deployed
Submillimeter Receiver Status
Focal plane arrays are critical for imaging – C/Hartley2 resolved with 3.4m dia Herschel at 557 GHz, as are most astronomical (ISM) sources
Technology for mixers (SIS & HEB) is mature; cooling to 4K is required. SIS to 1400 GHz and HEB above InP MMIC amplifiers available to 500 GHz but not yet competitive in terms of noise, but operate at 15 K
Frequency-multiplied tunable local oscillatorsLocal oscillators have made major advances since Herschel HIFI in terms of power output, efficiency, and tunability. Designs and configurations for 16 pixels @ 1.9 THz and more at lower frequencies are available
Low-power broadband digital signal processing Custom CMOS ASICs have transformed capability to analyze broad bandwidths in many pixels (including different bands) simultaneously
Highest frequency dropped firstBeam recollimated by ellipsoidal reflectorNext lowest frequency band dropped….
Arrays for each band16 to 64 pixelsConfiguration to be optimized – depending on mission profile
Spectrometer for Heterodyne Receivers
This has been an issue at mm/submm wavelengths because of required large bandwidth and multiplicity of lines
Solutions have included filterbanks (typically used on atmospheric sounders), chirp spectrometers (low power; used on planetary missions), and acousto-optical spectrometers (complex, heavy; used on SWAS (SMEX) and Herschel/HIFI)Digital signal processing, offering many advantages, is now feasible but FPGA approach is relatively power hungry (~4W/GHz BW)Ideal technology is custom VLSI using technology developed for cell phones and other communications systemsDr. Adrian Tang at JPL has unique partnership with UCLA team and Qualcomm for development of CMOS VLSI chips for NASA applications
“SPECTROCHIP II” has 750 MHz bandwidth, 512 spectral channels, includes digitizer, data accumulator, and USB output interface5x10cm size on board with support circuitry; 200mW DC power
Next generation (Dec 2015) will have ≥ 2 GHz bandwidth, 8K channels
Spectrochip II
A Full 1.5 GS/s spectrum analyzer chip in advanced 65nm CMOS was developed by UCLA’s high speed electronics lab.
Integrated 7b digitizers, offset and interleaving calibration functions, clock management system and vector accumulation.
256dsb/512ssb channel quadrature output with integrated USB 2.0 controller
Full SoC Die Photo Full SoC Block Diagram
Module Assembly
Water Mission SummaryA heterodyne-only mission devoted to study of water in the local universe can provide dramatically enhanced capabilities compared to Herschel/HIFI
6 – 6.8 m diameter aperture provides 3 to 4 times greater collecting area and thus this factor higher sensitivity for pointlike sources
22” FWHM beam width at 557 GHz; 6.5” FWHM at 1900 GHz
Frequency bands 500 – 570 GHz (H2O, H218O, HDO)
890 – 1150 GHz (H2O, H218O, HDO, OH+, H2O+,
H3O+
1700 - 2100 GHz (H3O+, [CII], [OI], HeH+, CO)
20% to 50% reduction in noise temperature for individual pixels
16 – 64 pixel arrays for observations of extended sources – up to 100 X faster imaging than Herschel HIFI
Simultaneous observations with all (3 or more) bands