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Attached Photo: NOAA CIMS rack assembly (Steve B., Eleanor W. Chris J.,Xiaoli S., Justin J.)

AEROMMA 05/09/23 Mission Daily Schedule

AEROMMA Plan of the Day, May 9, 2023
 
0630: Aircraft access starts
0700: ESPO on deck
1700: Aircraft access ends
 
Foreign National Escorts Schedule: FNs, please coordinate directly with your assigned escorts for arrival/departure from AFRC
Lab:
Morning: 
Xiaoli S. (Jeff Peischl)
 
Afternoon: 
Xiaoli S.: (Jeff Peischl)
 
Aircraft:
Morning: 
Justin J.: (Eleanor Waxman)
 
Afternoon:

AEROMMA 05/08/23 Mission Daily Schedule

Plan of the Day, May 8, 2023, AFRC
We hit the ground running on Monday morning, some of our colleagues are already on site.
 
As previously mentioned, to avoid long waits at the badging office, the arrival of personnel is being distributed as follows:
 
7:30 - 8:15am
Brown, Steven
Brock, Charles
Ahern, Adam
Peischl, Jeffrey
Rollins, Andrew
 
8:30 - 9:15am
Jernigan, Chris
Robinson, Michael
Waxman, Eleanor

Laser Imaging Nephelometer

Instrument Type: 
Point(s) of Contact: 

Particle Analysis By Laser Mass Spectrometry- Next Generation

The Purdue PALMS-NG instrument measures single-particle aerosol composition using UV laser ablation to generate ions that are analyzed with a time-of-flight mass spectrometer.  The PALMS size range is approximately 150 to >3000 nm and encompasses most of the accumulation and coarse mode aerosol volume. Individual aerosol particles are classified into compositional classes.  The size-dependent composition data is combined with aerosol counting instruments from Aerosol Microphysical Properties (AMP), the Langley Aerosol Research Group Experiment (LARGE), and other groups to generate quantitative, composition-resolved aerosol concentrations.  Background tropospheric concentrations of climate-relevant aerosol including mineral dust, sea salt, and biomass burning particles are the primary foci for the ATom campaigns.  PALMS also provides a variety of compositional tracers to identify aerosol sources, probe mixing state, track particle aging, and investigate convective transport and cloud processing.

*_Standard data products_**: *

Particle type number fractions: sulfate/organic/nitrate mixtures, biomass burning, EC, sea salt, mineral dust, meteoric, alkali salts, heavy fuel combustion, and other. Sampling times range from 1-5 mins.

*_Advanced data products_**:*

Number, surface area, volume, and mass concentrations of the above particle types. Total sulfate and organic mass concentrations. Relative and absolute abundance of various chemical markers and aerosol sub-components: methanesulfonic acid, sulfate acidity, organic oxidation level, iodine, bromine, organosulfates, pyridine, and other species.

Instrument Type: 
Aircraft: 
ER-2 - AFRC, ER-2 - AFRC, DC-8 - AFRC
Point(s) of Contact: 

Laser Induced Fluorescence – Sulfur Dioxide

The LIF-SO2 instrument detects sulfur dioxide at the single-part per trillion (ppt) level using red-shifted laser-induced fluorescence. It has operated on the WB-57 and Global Hawk aircraft in the UT/LS, as well as on the DC-8. Sulfur Dioxide is an important precursor for aerosols including nucleation of new particles globally and can be greatly enhanced in the stratosphere following explosive volcanic eruptions. An important implication of the Asian Monsoon is transport of aerosol precursors including SO2 into the lower stratosphere.

Instrument Type: 
Measurements: 
Point(s) of Contact: 

CSU QC-TILDAS Ammonia

Ambient ammonia (NH3) mixing ratios are measured in-situ using a flight-ready, closed-path, optical-based NH3 monitoring system. The CSU-NH3 instrument system consists of a combination of commercially-available and custom-built components including: 1) a commercially-available infrared absorption spectrometer that serves as the heart of the NH3 monitor, 2) a commercially-available inertial inlet that acts as a filter-less separator of particles from the sample stream, 3) a custom-built aircraft inlet, 4) a custom-designed vibration isolation mounting system for the spectrometer, and 5) an optional system for adding passivant to the sample stream.

The heart of the instrument is a closed-path, commercial (Aerodyne Research, Inc.), single-channel, quantum-cascade tunable infrared laser direct absorption spectrometer (QC-TILDAS) [McManus et al., 2010; McManus et al., 1995; Zahniser et al., 1995]. This spectrometer uses a direct absorption technique combined with a high sample flow rate (>10 SLPM) to achieve fast (up to 10 Hz) collection of absolute NH3 mixing ratios. The QC-TILDAS is operated with a heated aerodynamic separator (Aerodyne Research Inc., Inertial Inlet) that provides filter-less separation of particles >300 nm from the sample stream [Ellis et al., 2010]. An injection-style aircraft inlet allows calibration gases to be introduced into the sample stream within a few centimeters of the inlet tip. The custom inlet system is also designed to support the option for active continuous passivation of the sampling sufaces by 1H,1H-perflurooctylamine, a strong perfluorinated base that acts to coat the sampling surfaces with nonpolar chemical groups. Injection of this chemical into the aircraft inlet near the inlet tip prevents adsorption of both water and basic species on the sampling surfaces. The coating has been shown to greatly improve the instrument's time response in the laboratory and aboard research aircraft by increasing transmission of NH3 through the sample flow path [Pollack et al., 2019; Roscioli et al., 2016].

The QC-TILDAS is regularly calibrated on the ground and in flight via standard addition to the sample stream with a known concentration of NH3 generated from a temperature-regulated permeation tube (Kin-Tech), and zeroed by overflowing the inlet tip with a bottled source of NH3-free, synthetic air. The emission rate of the permeation device is calibrated before and after every mission by the NOAA ultraviolet optical absorption system [Neuman et al., 2003]. Allan variance analyses indicate that the in-flight precision of the instrument is 60 ppt at 1 Hz corresponding to a 3-sigma detection limit of 180 ppt. Zero signals span ±200 pptv, or 400 pptv total, with fluctuations in cabin pressure and temperature and altitude in flight. The total uncertainty associated with the 1-Hz measurement is ±(12% of the measured mixing ratio + 200 pptv).

The CSU-NH3 instrument has been successfully deployed (i.e. 100% data coverage) in two prior airborne research campaigns; one on the NSF/NCAR C-130 aircraft during the 2018 Western wildfire Experiment of Cloud Chemistry, Aerosol absorption and Nitrogen (WE-CAN) field campaign and the other aboard the University of Wyoming King Air during the TRANS2Am field campaign in 2019, 2021, and 2022. The aircraft inlet and aerodynamic separator are currently being modified in the laboratory to support lower pressure altitudes such as those anticipated for the full altitude range of the NASA DC-8 aircraft.

Instrument Type: 
Measurements: 
Aircraft: 
NSF/NCAR C-130, University of Wyoming King Air, DC-8 - AFRC
Point(s) of Contact: 

Cloud, Aerosol, and Refractive Index Experiment

CARE consists of three instruments: an Optical Particle AnaLyzer (OPAL), a second generation Cloud, Aerosol and Precipitation Spectrometer (CAPS), and a Precipitation Imaging Probe (PIP). CARE detects the size distributions of aerosol and cloud particles in the size range between 0.5 µm and 6.2 mm, provides information about particle shape and cloud phase, and allows the retrieval of refractive index of single particles in the size range between ~0.5 and 2 µm.

Aircraft: 
Point(s) of Contact: 

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