Long-term greenhouse gas measurements from aircraft

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Abstract

In March 2009 the NOAA/ESRL/GMD Carbon Cycle and Greenhouse Gases Group collaborated with the US Coast Guard (USCG) to establish the Alaska Coast Guard (ACG) sampling site, a unique addition to NOAA's atmospheric monitoring network. This collaboration takes advantage of USCG bi-weekly Arctic Domain Awareness (ADA) flights, conducted with Hercules C-130 aircraft from March to November each year. Flights typically last 8 h and cover a large area, traveling from Kodiak up to Barrow, Alaska, with altitude profiles near the coast and in the interior. NOAA instrumentation on each flight includes a flask sampling system, a continuous cavity ringdown spectroscopy (CRDS) carbon dioxide (CO 2)/methane (CH4)/carbon monoxide (CO)/water vapor (H 2O) analyzer, a continuous ozone analyzer, and an ambient temperature and humidity sensor. Air samples collected in flight are analyzed at NOAA/ESRL for the major greenhouse gases and a variety of halocarbons and hydrocarbons that influence climate, stratospheric ozone, and air quality. We describe the overall system for making accurate greenhouse gas measurements using a CRDS analyzer on an aircraft with minimal operator interaction and present an assessment of analyzer performance over a three-year period. Overall analytical uncertainty of CRDS measurements in 2011 is estimated to be 0.15 ppm, 1.4 ppb, and 5 ppb for CO2, CH4, and CO, respectively, considering short-term precision, calibration uncertainties, and water vapor correction uncertainty. The stability of the CRDS analyzer over a sevenmonth deployment period is better than 0.15 ppm, 2 ppb, and 4 ppb for CO2, CH 4, and CO, respectively, based on differences of on-board reference tank measurements from a laboratory calibration performed prior to deployment. This stability is not affected by variation in pressure or temperature during flight. We conclude that the uncertainty reported for our measurements would not be significantly affected if the measurements were made without in-flight calibrations, provided ground calibrations and testing were performed regularly. Comparisons between in situ CRDS measurements and flask measurements are consistent with expected measurement uncertainties for CH4 and CO, but differences are larger than expected for CO2. Biases and standard deviations of comparisons with flask samples suggest that atmospheric variability, flask-to-flask variability, and possible flask sampling biases may be driving the observed flask versus in situ CO2 differences rather than the CRDS measurements. © Author(s) 2013.

Figures

  • Fig. 1. Flight paths from the three complete seasons of GHG sampling: 2009 (left panel), 2010 (center panel), and 2011 (right panel). The color of the flight path corresponds to the month of the flight.
  • Fig. 2. NOAA equipment pallet for USCG C-130: three reference gas cylinders, instrument rack, and two Programmable Flask Packages (PFPs) (left). Window replacement inlet plate (external view) (right).
  • Fig. 3. Schematic diagram of CO2/CH4/CO/H2O sampling system on the C-130 aircraft.
  • Fig. 4. Transition times between different standard gases for CO2 (left), CH4 (center), and water vapor (right), from a laboratory test, with parameters as they are at ACG. CO transition times were too short to be measurable within the instrument noise and are not shown. The WMO-recommended compatibility of measurements for CO2 and for CH4 is shown in solid black lines at 0.1 ppm and 2 ppb, respectively. The solid black lines on the right panel indicate 0.01 %, or 100 ppm H2O.
  • Fig. 5. Transition times from wet to dry gas (red) and from dry to wet (green) before (dashed lines) and after (solid lines) the analyzer software parameter change that controls the baseline response time. CO2 is shown in the left panel and CH4 on the right. The WMO-recommended compatibility of measurements is shown in solid black lines: 0.1 ppm for CO2 and 2 ppb for CH4.
  • Table 1. Typical short-term precision of Picarro CRDS analyzers at the fastest measurement frequency (∼ 0.5 Hz). Flight condition values occur during turbulent portions of flights (i.e., low altitudes and/or altitude changes).
  • Table 2. Standard natural air reference tanks deployed for in situ calibration of the CRDS GHG analyzer, with their calibrated mole fraction values. Tanks were calibrated at NOAA/ESRL prior to deployment. Unless a specific date is indicated, the tank was in use for the entire season.
  • Fig. 6. Residuals of reference gas measurements for CO2 (left), CH4 (middle), and CO (right), during a flight on 4 April 2011. Different colors represent the different tanks, while the dashed black line is a linear fit with time to all the residuals. The dashed line is used to correct the sample mole fractions. Error bars are the standard deviation (1 s) of the 0.5-Hz measurements of the standard gas during the 2-min averaging time. Solid black lines represent the WMO compatibility goals.

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CITATION STYLE

APA

Karion, A., Sweeney, C., Wolter, S., Newberger, T., Chen, H., Andrews, A., … Tans, P. (2013). Long-term greenhouse gas measurements from aircraft. Atmospheric Measurement Techniques, 6(3), 511–526. https://doi.org/10.5194/amt-6-511-2013

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