Cloud Imaging Probe (CIP)

 

A state-of-the-art probe that provides images and comprehensive data on larger cloud particles.
Special Features: Grayscale imaging, Finer resolution, Anti-shatter tips (all optional)

 

 

Applications

  • Cloud particle research
  • Climate studies
  • Storm and hurricane research
  • Weather modification
  • Contrails and contrail-induced cirrus
  • Cloud chambers
  • Agricultural and industrial spray characterization

The CIP is suitable for fixed site, mobile or airborne sampling.

 

Photo at left: The CIP and other instruments mounted on a Russian research aircraft. Photo courtesy of the Central Aerological Observatory in Moscow. Photo at right: Columns, plates and aggregates recorded by researchers at Forschungszentrum Juelich.

 

Advantages

The CIP offers comprehensive particle data:

The CIP provides particle size distributions from 25 µm to 1550 µm, or 15-930 µm with optional 15-µm resolution.
The CIP’s 64 photodetectors generate high-quality images that allow for easy identification of particle types. The grayscale option (see "Optional Features") provides enhanced images based on the density in different regions of the particle.
The CIP records information on atmospheric temperature and pressure, aircraft velocity and altitude, and liquid water content (LWC) from 0.01 to 3 g/m3.

 

Optional Features

You can customize the CIP with several optional features:

Grayscale imaging provides detail about particle composition that is missed with monoscale imaging. In particular, grayscale imaging gives three levels of shadow recording on each photodetector as opposed to one. The pictures below show the same particles recorded with grayscale imaging (left) and monoscale imaging (right).

 

The CIP is offered in a 15 µm resolution as well as the standard 25 µm resolution.
The CIP can be purchased with special Korolev anti-shatter tips, shown below. Korolev tips significantly reduce the incidence of particle artifacts in the sample area.

 

 

Software

Two optional software packages are available  for CIP users. The Particle Analysis and Display System (PADS) allows for instrument control and real-time data display.

The second software package, the Optical Array Shadow Imaging Software (OASIS), facilitates post-processing particle analysis. More information about these two packages is given below.

 

Particle Analysis and Display System (PADS)

PADS displays a user-friendly virtual instrument panel that enables the user to do the following tasks:

  • Start data recording and sampling
  • View real-time particle image data 
  • View particle volume and number concentrations, as well as Median Volume Diameter (MVD) and Effective Diameter (ED)
  • View LWC as measured or calculated by the hotwire sensor and CIP
  • Monitor instrument parameters like CIP laser current and various electronics voltages
  • Play back data for post-flight viewing

Online CIP Software Manual

 

 

Optical Array Shadow Imaging Software (OASIS)

OASIS, shown at right, is designed for rigorous post-processing analysis. It provides additional particle statistics beyond those generated by PADS. In addition, OASIS allows users to filter particles by various criteria, including particle area, particle shape, area fraction, and inter-arrival time. Written in IGOR Pro, OASIS leverages IGOR’s robust statistical analysis features for enhanced data analysis and graphing capability. 

 

How it Works

Shadow images of particles passing through a collimated laser beam are projected onto a linear array of 64 photodetectors. The presence of a particle is registered by a change in the light level on each diode. The registered changes in the photodetectors are stored at a rate consistent with probe velocity and the instrument’s size resolution. Particle images are reconstructed from individual “slices,” where a slice is the state of the 64-element linear array at a given moment in time. A slice must be stored at each time interval that the particle advances through the beam a distance equal to the resolution of the probe.  Optional grayscale imaging gives three levels of shadow recording on each photodetector, allowing more detailed information on the particles. 

The CIP also contains a Hotwire LWC sensor.  This sensor estimates liquid water content using a heated sensing coil. The system maintains the coil at a constant temperature, usually 125 °C, and measures the power necessary to maintain this temperature. More power is needed to maintain the temperature as droplets evaporate on the coil surface and cool the surface and surrounding air. Hence, this power reading can be used to estimate LWC. Both the LWC design and the optional PADS software contain features to ensure the LWC reading is not affected by conductive heat loss.

Specifications

Parameter CIP Specification Specification for Included Hotwire LWC
Technique Optical Array Probe with 64 elements: 62 sizing elements, end diode rejection Temperature-Controlled Hotwire Sensor
Measured Particle Size Range 12.5 µm – 1.55 mm  (for 25-µm resolution CIP)
7.5 – 930 µm (for 15-µm resolution CIP)
N/A; measured LWC range is 0 - 3 g/m3
Sample Area Variable; depends on tip configuration and particle size N/A
Upper Concentration Range: Depends on particle size, but up to 500 particles/ cm3 for a CIP with standard tips and arm width 3 g/m3
Air Speed Range 10 – 300 m/sec (for 25-µm resolution CIP) 
10 - 180 m/sec (for 15-µm resolution CIP)
10 – 200 m/sec
Number of Size Bins 62

N/A

Sampling Frequency 1D histogram data: 0.05 to 25 Hz; 2D image data: variable interval, when buffer fills
Laser 658 nm, 30 mW
Calibration Verification: Spinning glass disk with opaque dots of known size Not required
Auxiliary Parameters Ambient Temperature, Relative Humidity, Static Pressure, Dynamic Pressure 
Data System Interface: 2D CIP data: RS-422, High Speed, 4 Mb/sec Baud Rate
System data: RS-232 or RS-422, 56.6 kb/sec Baud Rate
Optional Software: Particle Analysis and Display System (PADS) 
Optical Array Shadow Imaging Software (OASIS)
Weight: 21 lbs./9.5 kg in DMT canister
Power Requirements 28VDC: 11A for probe system, anti-ice heaters either 13A (standard tips) or 17A (Korolev tips)
Optional AC voltages for system power and anti-ice heaters
Environmental Operating Conditions Temperature: -40 °C to +40°C (-40 °F to +104 °F)
RH: 0 – 100%, non-condensing
Altitude: 0 - 50,000 ft
Routine Maintenance: DMT recommends conducting basic instrument performance checks and inspecting the CIP optical windows before a flight. A weekly calibration check is also recommended. 

Specifications are subject to change without notice.

 

Included Items

  • Instrument
  • Shipping case
  • Operator manual
  • One-year warranty
  • Spinning disk for calibration check (pictured)
  • One day of training at DMT’s facility
  • Email and telephone technical support

Accessories (Purchased separately)

  • Laptop and Particle Analysis and Display System (PADS) software
  • OASIS Software
  • Data Acquisition System

 

How to Order

Contact DMT for pricing or more information.

Email: customer-contact@dropletmeasurement.com

Phone: +001 303 440 5576
Fax: +001 303 440 1965

Selected Bibliography

Fairall, C. W., M. L. Banner, W. L. Peirson, W. Asher, and R. P. Morison (2009), “Investigation of the physical scaling of sea spray spume droplet production,” J. Geophys. Res., 114, C10001, doi:10.1029/2008JC004918. Link

Grosvenor, D. P., Choularton, T. W., Lachlan-Cope, T., Gallagher, M. W., Crosier, J., Bower, K. N., Ladkin, R. S., and Dorsey, J. R.: “In-situ aircraft observations of ice concentrations within clouds over the Antarctic Peninsula and Larsen Ice Shelf,” Atmos. Chem. Phys. Discuss., 12, 17295-17345, doi:10.5194/acpd-12-17295-2012, 2012. Link

Heymsfield, Andrew J., Carl Schmitt, Aaron Bansemer, Cynthia H. Twohy, 2010: “Improved Representation of Ice Particle Masses Based on Observations in Natural Clouds.” J. Atmos. Sci., 67, 3303–3318. Link

McBride, P. J., K. S. Schmidt, P. Pilewskie, A. Walther, A. K. Heidinger, D. E. Wolfe, C. W. Fairall, and S. Lance (2012), “CalNex cloud properties retrieved from a ship-based spectrometer and comparisons with satellite and aircraft retrieved cloud properties,” J. Geophys. Res., 117, D00V23, doi:10.1029/2012JD017624. Link

Min, Q., Joseph, E., Lin, Y., Min, L., Yin, B., Daum, P. H., Kleinman, L. I., Wang, J., and Lee, Y.-N.: “Comparison of MODIS cloud microphysical properties with in-situ measurements over the Southeast Pacific,” Atmos. Chem. Phys., 12, 11261-11273, doi:10.5194/acp-12-11261-2012, 2012. Link

Padmakumari B, Maheskumar RS, Morwal SB, Harikishan G. Konwar M, Kulkarni JR, Goswami BN. 2012. “Aircraft observations of elevated pollution layers near the foothills of the Himalayas during CAIPEEX-2009.” Q. J. R. Meteorol. Soc. 2012, DOI:10.1002/qj.1989. Link

B. Padmakumari, R.S. Maheskumar, G. Harikishan, J.R. Kulkarni & B.N. Goswami (2013): “Comparative study of aircraft- and satellite-derived aerosol and cloud microphysical parameters during CAIPEEX-2009 over the Indian region,” International Journal of Remote Sensing, 34:1, 358-373. Link