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ACT-America: Instruments

ACT-America will deploy high-quality, field-tested (TRL-8 (Technology Readiness Level) or higher) trace gas and meteorological instruments. The mix of remote and in situ sensors enables extensive spatial coverage of key variables. The C-130 instruments includes the Multi-Functional Fiber Laser Lidar for CO2 columns, range to ground and surface reflectance; the Cloud Physics Lidar for ABL (Atmospheric boundary layer) depths and atmospheric aerosols; Picarro cavity ring-down spectrometers for in situ CO2, CH4, water vapor, and carbon monoxide (CO); 2B Technologies for in situ ozone; Flasks for CO2, CH4, CO, carbonyl sulfide, and 14CO2; and an environmental suite for in situ pressure, temperature and winds. The UC-12 has the same in situ sensors save for winds. Towers utilize Picarros for in situ CO2 and CH4.

ACT-America science instruments.

Instrument
(Platform)

Variables
Measured

Sampling
Frequency

Data Latency
(Archiving)1

Purpose of
measurement

MFLL (C-130)

Column CO2 number density,
altimetry, surface reflectance

10 Hz

1 day (≤6 months)

Core GHG CO2 measurement
& ranging capability

CPL (C-130)

ABL height, aerosol distribution

2 Hz, 30m vertical resolution

1 day (≤4 months)

Transport model constraint, OCO-2
validation

Picarro Air (C-130 & B-200)

CO2, CH4, CO, H2O
mole fraction

1 Hz

1 day (≤4 months)

Core GHG measurements, combustion
& airmass tracer

2-B Tech. (C-130 & B-200)

O3 mole fraction

1 Hz

1 day (≤4months)

Airmass tracer

Atm. state and nav. (C-130)

GPS Lat.-Lon, Wind speed, direction,
Pressure, Temp.

1 Hz or higher

1 day (≤6 months)

Evaluate atmospheric transport models

Atm. State and nav. (B-200)

GPS Lat. and Lon., Pressure,
Temperature

1 Hz or higher

1 day (≤6 months)

Evaluate atmospheric transport models

Flasks (C-130 & B-200)

Multiple trace gases. See table 3-2

12 flasks / aircraft / flight

1 month

(≤6 months)

Core GHG measurements, GHG source
tracers.

Picarro Ground

CO2, CH4, H2O
mole fraction

1 Hz

1 day (≤6 months)

Core GHG measurements.

Science Instrumentation

The C-130 payload includes two remote sensing instruments: the Multi-Functional Fiber Laser Lidar (MFLL, Dobler et al. 2013), a Laser Absorption Spectrometer (LAS) for measuring CO2 column number density weighted to the near surface atmosphere as well as range to the surface and surface reflectance, and the Cloud Physics Lidar (CPL, McGill et al. 2002), an aerosol backscatter lidar for measuring ABL depth and aerosol distributions. The C-130 also carries a comprehensive suite of in situ sensors measuring CO2, CH4, carbon monoxide (CO), ozone (O3), and H2O (water), and flasks that measure CO2 and CH4 as well as GHG tracers, particularly CO, COS, and 14CO2. The B-200 has an identical suite of in situ sensors and flask sampling capability. In situ sensor redundancy for CO2, CH4 and CO on each aircraft provides the opportunity to evaluate in flight performance of the measurements. Both aircraft are also equipped to provide high accuracy and precision meteorological measurements. All instruments meet or exceed the precision and accuracy levels required by the STM over the requisite averaging scale. Most instruments exceed the STM requirements at their native resolutions, which are higher than those required by the STM.

Remote Sensing Instruments
MFLL: The MFLL is a suite of Continuous-Wave (CW) lidar instruments consisting of: 1) an intensity modulated multi-frequency single-beam synchronous-detection Laser Absorption Spectrometer (LAS) operating at 1571 nm for measuring the column amount of CO2 number density and range between the aircraft and the surface or to cloud tops, and surface reflectance; and 2) a Pseudo-random Noise (PN) altimeter at 1596 nm for measuring the path length from the aircraft to the scattering surface and/or cloud tops..

The LAS instrument, developed by Exelis, Inc. (now part of Harris Corp.) in 2004 (Dobler, et al., 2013, Lin, et al., 2013, Dobbs et al., 2007, 2008a), has been extensively evaluated in 1000+ hours of ground testing and in 13 multi-day flight campaigns conducted over a variety of meteorological conditions and surface types during both days and nights (Browell et al., 2008, 2009, 2012). The LAS CO2 column measurements have a precision of 0.08% for a 10-s horizontal average (~1.5 km on C-130) over land and 0.18% over water. These precision values are equivalent to relative CO2 mole fraction precisions of about 0.30 ppm and 0.72 ppm, respectively. Absolute comparisons of CO2 remote and in situ measurements showed an absolute accuracy of 0.65 ppm of CO2 (Dobler, et al., 2013, Browell et al., 2012), meeting the 1 ppm CO2 accuracy requirement. Based on this extensive flight testing, the LAS instrument meets the CO2 column measurement requirements of the mission and is considered to be at TRL-8.

CPL: The CPL is an airborne lidar system designed specifically for studying clouds and aerosols (McGill, et al., 2002), and has participated in nearly 30 science measurement campaigns (e.g. McGill et al., 2003, and McGill et al., 2004). It also has been used extensively for satellite validation (e.g., McGill et al., 2007 and Vaughan et al., 2010). The Cloud Physics Lidar provides a complete battery of cloud physics information, greatly surpassing the measurement requirements for ACT-America, especially for ABL height measurements. Data products include:

  • Cloud profiling with 30 m vertical and 200 m horizontal resolution at 1064 nm, 532 nm, and 355 nm, providing cloud location and internal backscatter structure.
  • Aerosol, boundary layer, and smoke plume profiling at all three wavelengths.
  • Depolarization ratio to determine the phase (e.g., ice or water) of clouds using the 1064 nm output.
  • Cloud particle size determined from a multiple field-of-view measurement using the 532 nm output (off-nadir multiple scattering detection).
  • Direct determination of the optical depth of cirrus clouds (up to ~OD 3) using the 355 nm output.

The CPL uses photon-counting detectors with a high repetition rate laser to maintain a large signal dynamic range. This dramatically reduces the time required to produce reliable and complete data sets. The goal of the CPL analysis is to provide data within 24 hours of a flight including the cloud and aerosol quick-look pictures, cloud boundaries, ABL height, and depolarization information. The final data release shall be within 4 months for the mission.

Airborne In Situ Instruments
Picarro continuous CO2/CH4/H2O/CO: The C-130 and B-200 both have Picarro instruments. The Picarro instruments have been extensively tested on aircraft flights (Karion et al., 2013a, b; Mays et al., 2009; Turnbull et al., 2011). Picarro analyzers are based on Wavelength-Scanned Cavity Ring Down Spectroscopy (WS-CRDS), a time-based measurement utilizing a near-infrared laser to measure a spectral signature of molecular absorption. Gas flows through a 35-cc optical cavity with an effective path length of up to 20 km and pressure of 140 Torr. Extremely stable and high-precision measurements are achieved through cavity temperature, pressure, and laser frequency control to better than 0.002 °C, 0.00003 atm and 1 MHz, respectively. Aircraft instruments are similar to surface-based sensors, but use faster flow rates, solid-state data storage, and additional vibration isolation. These instruments exceed the precision requirements of the STM for all four gases (Table 2, Karion et al., 2013a). Accuracies of 0.2 ppm for CO2 and 2 ppb for CH4 (Karion et al., 2013a) also exceed mission accuracy requirements of 1 ppm for CO2 and 4 ppb for CH4.

2B Technologies Continuous O3: The Model 205 O3 monitor uses two ultraviolet beams in two cells to simultaneously measure O3-scrubbed air and unscrubbed air. This model has been approved by the Environmental Protection Agency as a Federal Equivalent Method (FEM) and is the fastest UV-based O3 monitor available. The O3 monitor has been previously flown on tropospheric chemistry field missions and meets the accuracy and precision requirements laid out in the STM (Bertschi et al. 2004).

Flask Measurement System: The NOAA Earth System Research Laboratory (ESRL) carbon cycle group has developed programmable flask packages (PFP) used in their aircraft network since 2003 and the tall tower measurement network since 2006. The PFPs hold twelve 0.7-L silicate glass flasks that can be triggered manually or automatically at specific altitudes, times or locations. Measurements of CO2, CH4, CO and other trace gases are made on one of two nearly identical automated analytical systems; the same systems are used in the ESRL ground, tall tower, and aircraft networks (Conway et al., 1994; Dlugokencky et al., 1994; Novelli et al., 1998). COS (and hydrocarbons and halocarbons) will be measured via Gas Chromatography/Mass Spectrometry measurements. PFP flask sample responses are calibrated against whole air working reference gases, which, in turn, are calibrated with respect to gravimetric primary standards. At selected times, duplicate flasks will be collected and analyzed for 14CO2. Accuracy and precision for these measurements are 0.2 ppm for CO2, 2 ppb for CH4 (Karion et al., 2013a), 2 ppb for CO (Novelli et al., 1998), 2 ppt for COS (Montzka et al., 2007), and 2 per mil for 14CO2, matching or exceeding the STM accuracy and precision requirements.

Environmental Parameters Suite: Water vapor, pressure, and ambient temperature are measured on both aircraft. Wind direction and speed will be measured on the C-130 only. Water vapor will be measured using a 3-stage chilled mirror hygrometer to make dew/frost point measurements with an accuracy of 0.2 °C. Ambient temperature will be derived using a Rosemount non-deiced model 102 total air temperature probe with a precision of 0.2 °C. Horizontal and vertical winds on board the C-130 are calculated from high precision pressure transducers and aircraft position and attitude data generated by Honeywell inertial navigation positioning systems. Wind speed direction will be measured to within 5 degrees while horizontal winds will have an accuracy of ±1 m/s. Both measurements are made at 10-Hz intervals.

Surface Measurements
ACT-America will install five Picarro CO2/CH4/H2O instruments on existing communications towers, filling gaps that exist in or near our three study regions in the existing tower network. Specific sites will be selected in science-critical locations based on tall tower and local Ethernet or cell phone data connection availability. Data will be collected at 100 m above ground level (AGL) or higher. Daily, automated data transfer to the Langley Atmospheric Science Data Center will allow remote monitoring of instrument status and investigation planning. The tower-based investigators continuously operated five similar tower installations in the Midwest from 2007-2009 (Richardson et al., 2012b; Miles et al., 2012) and are currently operating 12 such installations around the city of Indianapolis (Miles et al., 2013). Additional measurements that will be used in this study include NOAA moorings along the East and Gulf coasts, the Total Carbon Column Observing Network (TCCON) sites at Park Falls, Wisconsin (WLEF) and the Department of Energy-Atmospheric Radiation Measurement (DOE-ARM) Central Facility, OK sites, and the NOAA Aircraft (biweekly vertical profiles) and Tall Tower networks. These data are all accessible to the public. ACT-America investigators have extensive background working with these networks and the responsible investigators and programs.

PurpleAir PA-II-SD Air Quality Sensor
Laser Particle Counters
Type (2) PMS5003
Range of measurement 0.3, 0.5, 1.0, 2.5, 5.0, & 10 μm
Counting efficiency 50% at 0.3μm & 98% at ≥0.5μm
Effective range
(PM2.5 standard)*
0 to 500 μg/m³
Maximum range (PM2.5 standard)* ≥1000 μg/m³
Maximum consistency error (PM2.5 standard) ±10% at 100 to 500μg/m³ & ±10μg/m³ at 0 to 100μg/m³
Standard Volume 0.1 Litre
Single response time ≤1 second
Total response time ≤10 seconds
Pressure, Temperature, & Humidity Sensor
Type BME280
Temperature range -40°F to 185°F (-40°C to 85°C)
Pressure range 300 to 1100 hPa
Humidity Response time (τ63%): 1 s
Accuracy tolerance: ±3% RH
Hysteresis: ≤2% RH


Pandora capabilities

Instrument

Response

Parameter

Precision

Uncertainty

Range

Resolution

Pandora

~2min

Total Column O3, NO2, HCHO, SO2, H2O, BrO

0.01 DU

0.1 DU

 

 

Virginia Department of Environment Quality in-situ instrumentation

Instrument

Response

Parameter

Precision

Uncertainty

Thermo Scientific 42C (Molybdenum converter)
(VADEQ)

60 s

NO and NOx

50 pptv

3%

Teledyne API 200EU w/ photolytic converter
(EPA) PI-Szykman

20 s

NO2

50 pptv

 

Thermo Scientific 49C (VADEQ)

20 s

O3

1 ppbv

4%

Thermo Scientific 48i (VADEQ)

60 s

CO

40 ppbv

5%

Thermo Scientific 43i (VADEQ)

80 s

SO2

0.2 ppbv

5%

Thermo Scientific 1400AB TEOM (VADEQ)

600 s

PM2.5 (continuous)

µg/m3

1 3%

Thermo Scientific Partisol Plus 2025 (VADEQ)

24 hr

PM2.5 (filter-based FRM)- 1/3 days

 

 

BSRN-LRC-49
Large area view.
Latitude: 37.1038
Longitude: -76.3872
Elevation: 3 m Above sea level
Scenes: urban, marsh, bay, river and farm.

Legend

  • The inner red circle is a 20km CERES foot print centered on the BSRN-LRC site.
  • The pink circle represents a possible tangential 20km foot print.
  • The middle red circle represents the area in which a 20km foot print could fall and still see the site.
  • Yellow is a sample 40 deg off nadir foot print.
  • The outer red circle is the region which would be seen by a possible 40 deg off nadir foot print.
The BSRN-LRC sun tracker at the NASA Langley Research Center on a snowy day (02/20/2015) The BSRN-LRC sun tracker at the NASA Langley Research Center on a snowy day (02/20/2015)
CAPABLE-BSRN Google Site Location Image

Team Satellite Sensor G/L Dates Number of obs Phase angle range (°)
CMA FY-3C MERSI LEO 2013-2014 9 [43 57]
CMA FY-2D VISSR GEO 2007-2014
CMA FY-2E VISSR GEO 2010-2014
CMA FY-2F VISSR GEO 2012-2014
JMA MTSAT-2 IMAGER GEO 2010-2013 62 [-138,147]
JMA GMS5 VISSR GEO 1995-2003 50 [-94,96]
JMA Himawari-8 AHI GEO 2014- -
EUMETSAT MSG1 SEVIRI GEO 2003-2014 380/43 [-150,152]
EUMETSAT MSG2 SEVIRI GEO 2006-2014 312/54 [-147,150]
EUMETSAT MSG3 SEVIRI GEO 2013-2014 45/7 [-144,143]
EUMETSAT MET7 MVIRI GEO 1998-2014 128 [-147,144]
CNES Pleiades-1A PHR LEO 2012 10 [+/-40]
CNES Pleiades-1B PHR LEO 2013-2014 10 [+/-40]
NASA-MODIS Terra MODIS LEO 2000-2014 136 [54,56]
NASA-MODIS Aqua MODIS LEO 2002-2014 117 [-54,-56]
NASA-VIIRS NPP VIIRS LEO 2012-2014 20 [50,52]
NASA-OBPG SeaStar SeaWiFS LEO 1997-2010 204 (<10, [27-66])
NASA/USGS Landsat-8 OLI LEO 2013-2014 3 [-7]
NASA OCO-2 OCO LEO 2014
NOAA-STAR NPP VIIRS LEO 2011-2014 19 [-52,-50]
NOAA GOES-10 IMAGER GEO 1998-2006 33 [-66, 81]
NOAA GOES-11 IMAGER GEO 2006-2007 10 [-62, 57]
NOAA GOES-12 IMAGER GEO 2003-2010 49 [-83, 66]
NOAA GOES-13 IMAGER GEO 2006 11
NOAA GOES-15 IMAGER GEO 2012-2013 28 [-52, 69]
VITO Proba-V VGT-P LEO 2013-2014 25 [-7]
KMA COMS MI GEO 2010-2014 60
AIST Terra ASTER LEO 1999-2014 1 -27.7
ISRO OceanSat2 OCM-2 LEO 2009-2014 2
ISRO INSAT-3D IMAGER GEO 2013-2014 2

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