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SOLVE Participants Discussing Instruments

Robert Hall Underneath ER-2

Lidar Atmosphere Sensing Experiment

The Differential Absorption Lidar uses the backscatter of two simultaneous laser wavelengths through zenith and nadir windows to measure the vertical profiles of H2O and aerosols/clouds.

NASA's Lidar Atmospheric Sensing Experiment (LASE) system is an airborne DIAL (Differential Absorption Lidar) system used to measure water vapor, aerosols, and clouds throughout the troposphere. LASE probes the atmosphere using lasers to transmit light in the 815-nm absorption band of water vapor. Pulses of laser light are fired vertically below the aircraft. A small fraction of the transmitted laser light is reflected from the atmosphere back to the aircraft and collected with a telescope receiver. The received light indicates the amount of water vapor along the path of the laser beam.

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Langley Aerosol Research Group Experiment

Langley Aerosol Research Group Experiment (LARGE).  The "classic" suite of instrumenation measures in-situ aerosol micrphysical and optical properties. The package can be tailored for specific science objectives and to operate on a variety of aircraft. Depending on the aircraft, measurments are made from either a shrouded single-diffuser "Clarke" inlet, from a BMI (Brechtel Manufacturing Inc.) isokinetic inlet, or from a HIML inlet. Primary measurements include:

1.) total and non-volatile particle concentrations (3nm and 10nm nominal size cuts),
2.) dry size distributions from 3nm to 5µm diameter using a combination of mobilty-optical-aerodynamic sizing techniques,
3.) dry and humidified scattering coefficients (at 450, 550, and 700nm wavelength), and
4.) dry absorption coefficients (470, 532, and 670nm wavelength). 

LARGE derived products include particle size statistics (integrated number, surface area, and volume concentrations for ultrafine, accumulation, and coarse modes), dry and ambient aerosol extinction coefficients, single scattering albedo, angstrom exponent coefficients, and scattering hygroscopicity parameter f(RH).

Aircraft: 
DC-8 - AFRC, C-130H - WFF, P-3 Orion - WFF, HU-25 Falcon - LaRC, King Air B-200 - LaRC, Twin Otter - CIRPAS - NPS
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Ozonesondes (NOAA)

NOAA Ozonesonde payloads include an Electrochemical Concentration Cell (ECC) ozonesonde, and a radiosonde to telemeter data to the ground and provide in situ measurements of temperature, pressure, relative humidity (surface to upper troposphere), and GPS coordinates. Sounding data typically reach an altitude of 28 km.

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Balloon
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Balloonsondes (NOAA)

NOAA Balloonsonde payloads include a NOAA Frost Point Hygrometer (FPH), an Electrochemical Concentration Cell (ECC) ozonesonde, and a radiosonde to telemeter data to the ground and provide in situ measurements of temperature, pressure, relative humidity (surface to upper troposphere), and GPS coordinates. Sounding data typically reach an altitude of 28 km.

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Aircraft: 
Balloon
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Balloon Borne Frost Point Hygrometer

The NOAA Balloon-borne Frost Point Hygrometer is based on the chilled mirror principle. The FPH measures the temperature of a small mirror controlled to maintain a constant, thin layer of frost. Under stable conditions the mirror temperature equals the frost point temperature of the air passing over the mirror. The frost coverage on the mirror is detected by a photodiode that senses the light of a light-emitting diode (LED) reflected off the mirror surface. Both optical components are rigorously temperature controlled, minimizing drift in the LED's intensity and the photodiode's sensitivity. The reflectance signal is used to control the temperature of the mirror using P-I-D logic. The mirror temperature is measured by a well-calibrated bead thermistor. The mirror temperature is telemetered to the ground station (along with a large array of other data) by a radiosonde that also provides in situ measurements of ambient temperature, pressure, relative humidity (only in the lower and middle troposphere), and GPS coordinates.

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Aircraft: 
Balloon
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