Mission Summary
20080912I1 Aircraft 43RF
EMC Tail Doppler Radar Operational Mission

Scientific Crew (43RF)
Lead Project ScientistJason Dunion
Radar/Workstation ScientistMike Black
Doppler ScientistNeal Dorst
AXBT ScientistBen Jaimes de la Cruz (UMiami)

Flight Crew (43RF)
PilotsBarry Choy
Amelia Ebhardt
Brian Taggart
Flight DirectorMarty Mayeaux
NavigatorsJoe Bishop
Ryan Kidder
Flt. Eng.Dewie Floyd
Data TechTerry Lynch
Dana Naeher
Jeff Smith
Elec. TechDamon Sans Souci

Mission Plan :

NOAA 43RF will participate in an EMC Tail Doppler Radar mission (with options to conduct HRD's TC-Ocean Interaction Experiment and SFMR shallow water module) into Hurricane Ike. The flight called for an initial IP well NE of the center. From the IP to a point north of the storm, NOAA 43 would fly at 5,000 ft (pressure altitude) to collect SRA data over the coastline. Following that long E-W leg, NOAA 43 would climb to 8,000 ft (pressure altitude) and begin a N-S leg south of Marsh Island, LA with a series of GPS dropsondes/AXBTs for HRD's SFMR shallow water module to investigate shoaling effects on SFMR retrieved winds. Finally, a rotated figure four pattern will be conducted. Since Ike's wind field had expanded quite a bit since the previous missions, the leg lengths were extended to ~120 nm. GPS dropsondes would be launched in the center, in areas with insufficient scatterers to derive Doppler winds and in selected locations where AXBTs will be launched. AXBTs and AXBT/GPS dropsonde combos will be targeted in areas of potential shoaling, locations coincident with a pre-storm ocean survey mission flown on 08 September as well as with NOAA drifting buoys in the area. Doppler wind and Super Ob analyses will be transmitted off the plane in real-time, if possible. The flight track, 17 GPS dropsonde points and 20 AXBT points are shown in Fig. 1. The flight track with overlaid tracks and positions of NOAA drifting buoys that were deployed ahead of the storm are shown in Fig. 2


Fig. 1: Flight track (red line) for EMC Tail Doppler Radar mission 20080912I1. GPS dropsondes, AXBTs and AXBT/GPS dropsonde combos that were launched are indicated by black circles, white circles and circled crosses respectively. The blue circle indicates the position of a NOAA drifting buoy that was overflown with a GPS dropsonde/AXBT combo.


Fig. 2: Flight track (white line) for EMC Tail Doppler Radar mission 20080912I1. The black circles show the positions of several NOAA drifting buoys that were launched ahead of the storm. Hurricane Ike's forecast track is shown by the black line with forecast points (yellow circles). Altimeter- derived ocean heat content values are indicated by the colored shading.

Mission Summary :

Take off Landing
MacDill AFB, FL10:32 UTC MacDill AFB, FL19:03 UTC

  1. Synoptic Situation

    On 12 August, Hurricane Ike was positioned on the southwest side of a deep layer ridge that was centered over the southeast U.S. (Fig. 3, left). Vertical wind shear analyses from UW-CIMSS indicated ~10-20 kt of shear over Ike (Fig. 3, right). Figures 3 and 4 also indicate that northeasterly shear was now present over the storm and that upper-level outflow appeared to be improving, though it was somewhat restricted on the east and northeast sides of the storm.


    Fig. 3: (Left) plot of 250-850 hPa deep layer mean steering [magnitude (direction) of the steering flow is indicated by colored shading (white streamlines) and the storm center is shown by the red hurricane symbol] for 12 Sept 1200 UTC. (Right) vertical wind shear [magnitude (direction) of the wind shear is indicated by yellow contours (orange streamlines)]) for 12 Sept 1200 UTC. Images courtesy of UW/CIMSS.


    Fig. 4: Plot of mid to upper-level GOES water vapor winds for 12 Sept 1200 UTC. Image courtesy of UW/CIMSS.

  2. Mission Specifics

    After a 2.5 hour delay (problems closing the APU hatch on NOAA 43), take-off was from MacDill at 1032 UTC. Hurricane Ike was located at ~26.9°N 92.2°W, its intensity was 90 kt (954 hPa) and its forward motion was 290 degrees at 11 kt. Figure 5 (left) shows an overpass by AMSR-E on the Aqua (89 GHz) satellite and indicates that Ike's convection continued to be quite asymmetric. Ike had a broad crescent shaped outer eyewall that was confined to the south and southeast portion of the storm. The AMSR-E 89 GHz image and NOAA 43's LF radar indicated that the small inner eyewall that had been present for the past few days had eroded, leaving behind a large eye. The TRMM Precipitation Radar confirmed the asymmetry seen in the AMSR-E 89 GHz image and indicated that high rain rates were virtually nonexistent in Ike's NW quadrant. Additionally, HRD H*Wind surface wind analyses conducted at 1330 UTC (not shown) indicated that Ike's wind field was continuing to expand.


    Fig. 5: Plots of (left) Aqua AMSR-E 89 GHz imagery for 12 Sept 0743 UTC and (right) TRMM Precipitation Radar imagery for 12 Sept 1034 UTC.

    The 8.5 hour flight pattern was executed as planned, except that the last center to NE leg was cut short (from 120 nm to 100 nm) to conserve extra fuel that was burned during the long 5,000 ft pressure altitude portion of the mission. The subsequent NW to center leg was therefore also shorter than outlined in the original mission plan (from 120 nm to 100 nm). There were six GPS dropsonde/AXBT combos and one overflight of a NOAA drifting buoy (with a GPS dropsonde/AXBT combo) was made at drop #17. The lowest GPS dropsonde pressure observed during the mission was 954.8 hPa at drop #10, during a pass through the center at 1308 UTC. Two Doppler wind analyses were transmitted off the P-3 in real-time during this mission. No Super Ob analyses were transmitted since the Super Obs were not being assimilated in real-time that day.

Problems :

Though there were no major problems during the flight, there were problems, including:

Jason Dunion
29 April 2009


Mission Data :

Dropsonde plots
850 mb
925 mb
1000 mb
surface

Flight-level Data

NetCDF listing

1 second listing


Flight track

Temperature and Moisture

Wind and Atlitude

Flight track detail


Page last updated April 29, 2009
Return to Mission page.