Handout (337.2 kB)
The LWC instruments included four hot-wire type devices (PMS King, Nevzorov, DRI large and small T-probes), optical scattering probes (FSSP-100), optical array probes (PMS 2D-C, 2D-P, 260-X), HVPS (High Volume Precipitation Spectrometer), Cloud Particle Imaging probe (CPI), and a counter-flow virtual impactor (CVI). The Nevzorov and DRI T-probes also measure ice water content (IWC). A Rosemount icing detector (RICE) detected supercooled liquid water. These instruments were on the fuselage and under-wing locations as shown in the top of Figure 1.
This paper describes the instrumentation, shows examples of the measurements, and identifies regimes where there were systematic differences in the LWC measurements. These differences arise from the range of drop sizes, the affect of probe location on the aircraft (fuselage, under-wing, wing-tip, pod), time response, and sub-cloud scale structure. The bottom of Figure 1 shows an example of observations from ten minutes of level flight (2.8 km MSL). It illustrates both the relative agreement and discrepancies among probe types.