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Design, characterization, and first field deployment of a novel aircraft-based aerosol mass spectrometer combining the laser ablation and flash vaporization techniques

MPS-Authors
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Hünig,  Andreas
Particle Chemistry, Max Planck Institute for Chemistry, Max Planck Society;

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Appel,  Oliver
Max Planck Institute for Chemistry, Max Planck Society;

/persons/resource/persons241660

Dragoneas,  Antonis
Particle Chemistry, Max Planck Institute for Chemistry, Max Planck Society;

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Molleker,  Sergej
Particle Chemistry, Max Planck Institute for Chemistry, Max Planck Society;

/persons/resource/persons230428

Clemen,  Hans-Christian
Particle Chemistry, Max Planck Institute for Chemistry, Max Planck Society;

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Helleis,  Frank
Max Planck Institute for Chemistry, Max Planck Society;

/persons/resource/persons101066

Klimach,  Thomas
Multiphase Chemistry, Max Planck Institute for Chemistry, Max Planck Society;

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Köllner,  Franziska
Particle Chemistry, Max Planck Institute for Chemistry, Max Planck Society;

/persons/resource/persons266285

Böttger,  Thomas
Particle Chemistry, Max Planck Institute for Chemistry, Max Planck Society;

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Drewnick,  Frank
Particle Chemistry, Max Planck Institute for Chemistry, Max Planck Society;

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Schneider,  Johannes
Particle Chemistry, Max Planck Institute for Chemistry, Max Planck Society;

/persons/resource/persons100858

Borrmann,  Stephan
Particle Chemistry, Max Planck Institute for Chemistry, Max Planck Society;

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Citation

Hünig, A., Appel, O., Dragoneas, A., Molleker, S., Clemen, H.-C., Helleis, F., et al. (2021). Design, characterization, and first field deployment of a novel aircraft-based aerosol mass spectrometer combining the laser ablation and flash vaporization techniques. Atmospheric Measurement Techniques Discussions, 14. doi:10.5194/amt-2021-271.


Cite as: https://hdl.handle.net/21.11116/0000-0009-5F82-A
Abstract
In this paper, we present the design, development, and characteristics of the novel aerosol mass spectrometer ERICA (ERC Instrument for Chemical composition of Aerosols) and selected results from the first aircraft-borne field deployment. The instrument combines two well-established methods of real-time in-situ measurements of fine particle chemical composition. The first method is the single particle laser ablation technique (here with a frequency-quadrupled Nd:YAG laser at λ = 266 nm). The other method is a combination of flash vaporization and electron impact ionization (like the Aerodyne aerosol mass spectrometer). The aerosol sample can be analyzed with both methods, each using time-of-flight mass spectrometry. By means of the laser ablation, single particles are qualitatively analyzed (including the refractory components) while the flash vaporization and electron impact ionization technique provides quantitative information on the non-refractory components (i.e., particulate sulfate, nitrate, ammonia, organics, and chloride) of small particle ensembles. These techniques are implemented in two consecutive instrument stages within a common sample inlet and a common vacuum chamber. At its front end, the sample air containing the aerosol particles is continuously injected via an aerodynamic lens (ADL). All particles which are not ablated by the Nd:YAG laser in the first instrument stage continue their flight until they reach the second instrument stage and impact on the vaporizer surface (operated at 600 °C). The ERICA is capable of detecting single particles with vacuum aerodynamic diameters (dva) between ~ 180 nm and 3170 nm (d50 cut-off). The chemical characterization of single particles is achieved by recording cations and anions with a bipolar time-of-flight mass spectrometer (B-ToF-MS). For the measurement of non-refractory components, the particle size range extends from approximately 120 nm to 3.5 µm (d50 cut-off; dva), and the cations are detected with a C-ToF-MS (compact time-of-flight mass spectrometer). The compact dimensions of the instrument are such that the ERICA can be deployed on aircraft, ground stations, or mobile laboratories . During its first deployments the instrument operated fully automated during 11 research flights on the Russian high-altitude research aircraft M-55 Geophysica from ground pressure and temperature up to 20 km altitude at 55 hPa and ambient temperatures as low as −86 °C.