Instrument Acronym:
VIPS
Instrument Measurements:
a) Trace Gas
b) Cloud Physics/Aerosol
The VIPS is an electro-optical instrument used to collect and record
a continuous sample of cloud particles down to 5 um. Particles are
collected continuously on a looped belt coated with silicone oil. The
portion of the belt exposed to the airstream is imaged by two very
hihg resolution charged coupled device (CCD) shuttered video cameras
with different resolutions. The resulting imagery is available for
real-time, in-flight evaluation of cloud conditions and for
post-flight habit classification and spectra analysis.
The VIPS system is composed of two parts: (1) an electro-optical collection and imaging unit mounted in a standard particle measurement system (PMS) can, and (2) data acquisition and recording components. Aperture width of the collection subassembly is adjustable for varying flight conditions. The CCD imaging cameras are coupled with inline, high detail video enhancers. Particle imagery is recorded continuously at 30 Hz on high-resolution Hi-8 VCRs. Images are also captured at 1 Hz, digitized in real-time and recorded on an Apple PowerPC.
c) Radiation/Optical/Electrical
d) Additional Capabilities
Real-time, in-flight evaluation if cloud conditions.
Resource Person/Developer:
Name: Andy Heymsfield
Affiliation: NCAR
Phone: (303) 497-8943
Email: heyms1@ucar.edu
Principle of Measurement:
In situ/Remote/Flux Measurement:
Field projects in which the instrument has been used:
WAVE90, FIRE-II, TOGA COARE, CEPEX, ARM, SUCCESS
McFarquhar, G.M., and A.J. Heymsfield, 1996: Microphysical characteristics of three anvils sampled during the Central Equatorial Pacific Experiment. J. Atmos. Sci., 53, 2401-2423.
Aircraft Platform:
Inlet Configuration/Location:
Collection/imaging unit in standard PMS can; Acquisition/recording
unit is cabin-mounted
Calibration/Cross Calibration:
NIST-traceable galss beads; stage micrometer
Operator Requirements:
Changing video tapes every two hours
Data Collection:
self
Post-flight Data Validation, Processing, Hours per Flight Hour etc.
Semi-automated analysis by computer
Physical Characteristics:
Dimensions: collection/imagin unit fits in standard PMS can
Weight: 5.9 kg
Power: collection/imaging unit: 28 VDC; acquisition/recording unit 115 VAC
Other:
Response Time:
continuous
Detection Limits:
5 um lower detection limit
> 150 um upper detection limit
Accuracy:
5 to > 150 um diameter
± 10 um
Precision:
± 1-2 um
Limitations (such as altitude, airspeed, etc.)