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Synonyms: 
Cessna Citation II
Associated content: 

MOPITT Airborne Test Radiometer

The MOPITT Airborne Test Radiometer (MATR) is a gas correlation filter radiometer that was developed to support and validate the MOPITT satellite program. It is a scaled-down version of the MOPITT instrument that comprises two thermal channels near 4.6 µm for measuring CO and one solar channel near 2.33 µm (or 2.27 µm) for measuring CO (or CH4). Inasmuch as its spatial resolution (1.2 km x 1.2 km) is much higher than that of the MOPITT radiometer (22 km x 22 km), MATR measurements provide an opportunity to look at the horizontal distribution of CO in more detail, which is especially useful for investigating localized pollution sources.

Instrument Type: 
Measurements: 
Aircraft: 
Point(s) of Contact: 
John Gille (Prev PI)

Cessna Citation II

UND Citation
Owner/Operator: 
University of North Dakota
Type: 
Conventional aircraft
Duration: 
7.0 hours (payload and weather dependent)
Useful Payload: 
2 852 lbs
Gross Take-off Weight: 
14 500 lbs
Max Altitude: 
43,000 MSL
Air Speed: 
348 knots
Range: 
1 998 Nmi

Continuous Flow Diffusion Chambers

The continuous flow diffusion chambers are oriented for vertical flow through an annular space. They are constructed of two cylindrical, thin, ebonized copper walls that are separated by approximately 1.1 cm. The walls of the CFDC are force-cooled either by circulating coolant through copper tubing coils surrounding the outer wall and inside the inner wall (laboratory CFDC) or by using these same coolant coils as evaporators for refrigeration compressor units (aircraft CFDC). In operation, the walls are coated with ice, achieved by flooding the chamber with water. An inlet manifold directs sample air containing aerosol particles into the center of a laminar flow field where the sample is surrounded on either side by particle-free sheath air (or N2). By varying the set temperatures of the two walls, the warm wall provides a vapor source to the cold wall so that water vapor and temperature fields are created. These fields and airflow determine the conditions of exposure for the aerosols during their typical 5 to 20 s residence time in the CFDC. Ice particles grow to relatively large sizes compared to aerosol particles and are distinguished from them using an optical particle counter (0.4 to 20 mm) at the base of the CFDC.

The aircraft CFDC transitions to a hydrphobic warm wall surface in the lower third of the device so that liquid water drops formed at RH>100% will evaporate, leaving only ice crystals as large particles. The only other physical differences between the two devices is the fact that the laboratory CFDC is approximately 50% longer, providing additional ice crystal growth time at ambient lab pressures and the laboratory device has associated equipment for aerosol generation and preconditioning.

An impactor is sometimes used following the optical counter to collect ice crystals onto specialized transmission electron microscope (TEM) grids for analysis of the residual particles. Calculations of air flow, temperature, and humidity are made assuming steady-state conditions (Rogers, 1988). The temperature and supersaturation range are determined by wall temperatures and air flow.

Instrument Type: 
Point(s) of Contact: 

C-130 Aircraft in Hangar

C-130 in Aircraft Hangar

C-130 Aircraft in Hangar During Integration

C-130 in Hangar During Integration

Instrument on ER-2 Aircraft

TSI 3563 Integrating Nephelometer

TSI Integrating Nephelometers are designed specifically for studies of direct radiative forcing of the Earth’s climate by aerosol particles, or studies of ground-based or airborne atmospheric visual air quality in clean areas. They may also be used as an analytical detector for aerosol particles whenever the parameter of interest is the light-scattering coefficient of the particles after a pretreatment step, such as heating, humidification, or segregation by size. The light-scattering coefficient is a highly variable aerosol property. Integrating Nephelometers measure the angular integral of light scattering that yields the quantity called the aerosol scattering coefficient, which is used in the Beer-Lambert Law to calculate total light extinction.

Measurements: 

High Volume Precipitation Spectrometer

SPEC previously built the Version 1 and Version 2 HVPS probes that have now been discontinued due to obsolete parts and significant advances in technology. The HVPS-3 uses the same 128-photodiode array and electronics that are used in the 2D-S and 2D-128 probes. The optics are configured for 150 micron pixel resolution, resulting in a maximum field of view of 1.92 cm (i.e., particles up to 1.92 cm are completely imaged, although even larger particles can be sized in the direction of flight).

Sample volume of the HVPS-3 is 400 L s-1 at 100 m s-1. The 2D-S or 2D-128 and HVPS make an excellent pair of probes that completely image particles from 10 microns to 1.92 cm.

Point(s) of Contact: 

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