The inter-comparison was facilitated by mounting the UA fuselage and a single wing to the NSSL-MM instrument rack such that the wing-mounted temperature/humidity and wind sensors could collect observations contemporaneous with the NSSL-MM sensors and within a nearly identical air stream. By incorporating the fuselage and wing, potential effects of the airframe on the sensors would be included in the observations. Although the NSSL-MM and Tempest-borne sensors could be compared without the NSSL-MM parent vehicle, mounting both systems to the vehicle enabled the investigators to 1) examine sensor sensitivity in a variety of atmospheric phenomena (these phenomena could be “chased”) and 2) examine the impact of the parent vehicle on the airstream within which both sensors resided.
During AVIATE, multiple transects across atmospheric airmass boundaries were executed. Response times of the temperature and humidity sensors were found to be similar but notable differences will be discussed along with the implications of response differences for the characterization of near-surface baroclinicity. The most significant impact of precipitation on the temperature/humidity sensors was observed when the vehicle entered and exited precipitation and therefore this impact is presumed to be a consequence of differences in the relative humidity sensor responses. Analysis of the measured winds along with numerical experiments designed to test hypotheses concerning the impact of the NSSL-MM parent vehicle on the flow field and wind sensors are underway.