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Diode Laser Hygrometer (DLH) Data and Instrument Status. Glenn Diskin, Tom Slate, Mario Rana NASA LaRC Jim Podolske NASA ARC ATTREX Science Team Meeting Boulder, Colorado October 23-25, 2013. Diode Laser Hygrometer (DLH) - description.
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Diode Laser Hygrometer (DLH)Data and Instrument Status Glenn Diskin, Tom Slate, Mario Rana NASA LaRC Jim Podolske NASA ARC ATTREX Science Team Meeting Boulder, Colorado October 23-25, 2013
Diode Laser Hygrometer (DLH) - description • Open-Path tunable diode laser spectrometer operating in the 1.4 µm spectral region • Uses commercial telecom fiber-coupled laser • Similar to previous versions of DLH, but built specifically for ATTREX, with new features • Wavelength modulation at ~2 kHz • Data analysis based on 2F, 4F demodulation, normalized by signal power • Line-locked to absorption line in low-pressure reference cell • Laser wavelength scanned periodically to determine laser-generated harmonic offsets • Uses one of three absorption lines, depending on conditions (primarily concentration), plus an altitude-dependent modulation • Double-pass external path configuration • “Mirror” is panel of retroreflecting roadsign material on wing-mounted fin • Sample volume is primarily outside of aircraft boundary layer • Internal optical path is pressurized and purged with dry air • No inlet effects, such as condensation, evaporation, hysteresis, etc. • Long path-length, combined with line-locked, multi-harmonic detection provideexcellent sensitivity and rapid time response • Normalization by return power allows measurements to be made within clouds • Cloud extinction can be assessed from return power signal (not done yet for ATTREX) • Real-time mixing ratio determination using onboard pressure, temperature • During ATTREX-2 (2013), internal correction applied to real-time data
DLH Installation on Global Hawk External Path 12.22 m RT Internal Path 0.55 m 27 7 18U 65 1 16 14 12 46 24 61 3 Zone 25
DLH Optical Housing - Internal Path Internal Path larger than on previous installations - Accommodates offset to Global Hawk lower fairing - Includes actuated folding mirror to allow for in-flight adjustment of beam path DLH Optical Housing Humidity Assessment - Internal Optical Path Measurement - Vaisala DMT152 New During ATTREX-2 / 2013 - Coupling to Global Hawk fairing rigid, leak-free - Optical Housing pressurized during flight * Purge/Refill cycling on demand * Reduced sensitivity to internal moisture - Mixing fans added to improve internal homogeneity and aid in moisture removal
DLH Data Status – ATTREX-2 • R0 data in ATTREX archive for all six science flights, R1 processing underway • R1 data use improved modulation assessment based on data acquired in AIDA chamber during AquaVIT2 • Data from ATTREX-1 will be reprocessed as well • Data cover entire range of altitudes and concentrations encountered • Data coverage is generally complete, with short calibration events every 30 minutes used to determine laser-induced harmonic offsets • Instrument signal to noise was very good; signal to internal background was much improved from ATTREX-1, and effect of internal humidity is measured and largely corrected • For R0 and R1 data, direct subtraction is used; still see what looks like residual early in each flight • Will investigate correcting using 2F/4F sensitivity differences, as was done for MACPEX
DLH Data Examples -- comparison with NOAA WV Science Flight 5 (2013/02/26) Science Flight 6 (2013/03/01) Thanks to NOAA WV group for pre-release copy of R1 data
Performance Issues Found in ATTREX-2,and Plans for Mitigation • Effects of internal humidity are still seen, early in flights, although magnitude is much improved from ATTREX-1 • More aggressive pre-flight purging of Optical Housing • Including adding / repositioning stirring fans • Purging of Electronics / Laser Chassis • Utilization of in-fiber sensor to separate effects from the two volumes • Utilization of multiple harmonics to further reduce impact on signal • Expect moisture control to be even more important flying from Guam • Will need larger supply of UZ Air than in ATTREX-2 • Internal Path optical alignment degraded in flight, reducing signal to noise of that component • Redesigned mounting of breadboard to decouple from optical housing flexure • Insufficient time to implement redesign; will use simpler mounting strategy instead for ATTREX-3