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Gulfstream IV-SP (G-IV)

Picture of Gulfstream IV-SP (G-IV)

The Gulfstream IV-SP (G-IV) is a high altitude, high speed, twin turbofan jet aircraft acquired by AOC in 1996. The G-IV is currently configured for operational support of the National Hurricane Center synoptic surveillance mission and is expected to provide support for NOAA programs for many years to come. This mission is designed to collect, process and transmit vertical atmospheric soundings in the environment of the hurricane. The principle tool used for this task is the GPS dropwindsonde.

The dropsonde is released from the G-IV measuring and transmitting back to the aircraft the pressure, temperature, humidity, and GPS Doppler frequency shifts as it descends to earth. The Doppler shifts are used to compute the horizontal and vertical wind components. After analysis and processing of the dropsonde data the information is formatted into a TEMP-DROP message using the standard WMO format. The TEMP-DROP message is then transmitted to the National Centers for Environmental Prediction and the National Hurricane Center for inclusion into the global and hurricane model runs. The TEMP-DROP message is also provided to the hurricane forecaster providing real-time observations depicting the synoptic patterns surrounding the hurricane.

Picture of Gulfstream IV-SP (G-IV)

Gulfstream G-IV SP (Special Performance)

Gulfstream G-IV SP Transformation Article

STANDARD AIRCRAFT SPECIFICATIONS

Engines: Two Fuselage Mounted Rolls Royce Tay 611-8 twin spool turbofan jet engines
Crew: (Hurricane and Winter Storm Missions):
2 pilots
1 flight engineer/mechanic
1 flight meteorologist (flight director)
1 High Altitude Profiling System (HAPS) system operator (can be automated)
3 Engineering Technicians/Dropwindesonde (Sonde) system operators
Ceiling: 45,000 feet
Rate of Climb (approximate - fully loaded): 3000 fpm (first 25000 ft.)
1500 fpm (through 33000 ft.)
1000 fpm (to 41,000 ft. – max wt. ceiling)
Operational Airspeeds: 41,000 – 45,000 ft. True Airspeeds (Mach .77-.80, 440-460 kts.)
Electrical: Two engine driven alternators (36KVA, 115 volt, unregulated 3 phase)
One Auxiliary Power Unit (APU) (36KVA, 115 volt, 400Hz, 3 phase)
Two Converters (converts and regulates engine alternator power)
Each provides: 23KVA, 400Hz, 3 phase AC power
250 amps, 28 volts DC power
Scientific Power: SED has an Uninterruptable Power Source (UPS) for scientific gear
Max. Gross Weight: Ramp 75,000 pounds
Takeoff 74,600 pounds
Landing 66,000 pounds
Empty Weight: 43,700 pounds
(operational configuration)
Useful Load: 31,300 pounds
(operational configuration)
Fuel Load: 29,500 pounds
Type Fuel: Jet A, JP4, JP5, JP8
Standard Fuel Burn: (fully loaded) = 5000 pounds/hr for first hour and 3000 pounds/hr for every hour after that
Maximum Range: 3800 nm. (with a 1 hour fuel reserve)
Maximum Duration: 8 hrs. 45 minutes (with 1 hour fuel reserve)
External Dimensions: Radome to trailing edge of horizontal stabilizer = 87.58 ft.
Radome to aft end of fuselage = 78.83 ft.
Wing Span = 77.83 ft.
Horizontal Tail Span = 32 ft.
Vertical Tail Height = 24.4 ft
Internal Dimensions: Head Room = 6ft.
Bulkhead to Bulkhead = 8 ft.
Cabin Length (Cockpit to Baggage Comp.) = 33 ft.
Useable Volume: Usable Length = 33 ft.
Usable Width = 6 ft.
Usable Height = 4 ft.
Usable Volume = 792 cubic ft.
Additional Standard Equipment
Cockpit: 2 High Frequency (HF) Radios
2 VHF Radios
Honeywell SATCOM Phone
GPS and Inertial Reference Systems (IRS) for navigation
1 UHF Radio
Honeywell TCAS II System (with FAA Change 7)
EROS Quick Donning Oxygen System
Collins WXR-700C (C-band weather radar)
Cabin: Dropwindesonde Tube with 8-channel tracking capability
Satellite Communication System with voice/data transmission capability
Numerous Computer Systems

The specific equipment and systems onboard the G-IV for the hurricane surveillance mission are the:

  • Main Aircraft Data System

- Two Data System Modules for instrument interface and data collection
- Four Networked Sun Sparc5 Workstations
- Extensive atmospheric instrumentation

  • Airborne Vertical Atmospheric Profiling System

- Dropsonde Data System for drop execution, data collection and storage
- Dropsonde Launch Chute
- GPS dropwindsonde

  • Hurricane Analysis and Processing System

- Workstation accomplishes data analysis, processing, and message formatting

  • Internal/External communication system

- VHF, UHF, ADF, Flight Phone, SATCOM and Passenger Communication System

  • Rockwell Collins WXR-700C C-Band Weather Radar w/ 30-inch antenna

The G-IV aircraft is on standby or deployed 180 days for hurricane surveillance, another 30-60 days are required for instrumentation and calibration, and 30 days for maintenance and training while anticipating between 200 to 300 hours of flying every year.

NOAA G-IV Winter Storms Reconnaissance

In order to more accurately predict the location and intensity of high winds, destructive surf conditions, severe weather and flooding rainfall caused by winter storms, the NOAA National Centers for Environmental Prediction (NCEP) instituted the Winter Storms Reconnaissance (WSR) program in 1998. Each year since then, the NOAA G-IV has served WSR from bases in Anchorage, AK and Honolulu, HI. In 2003, the G-IV will base from Hawaii, conducting approximately 20 missions over the North Pacific, into the breeding grounds of these future US-bound storms.

Over the years, NOAA NCEP has developed a method called targeted observations, whereby the NOAA jet is directed in advance to regions of the atmosphere where storm prediction models indicate enhanced data will have the most positive influence on the forecast accuracy. Once over these locations, dropwindsondes are launched to provide vertical soundings of the atmosphere between the aircraft and the ocean’s surface. Targeted observations have proven themselves in more than 90% of storm cases, generally improving the accuracy of storm track and intensity prediction between 10% - 20%. Another way to judge the public impact is that quantitatively, these additional observations from the G-IV result in giving emergency managers an extra day’s notification in which to declare warnings of severe weather events ahead.Picture of Gulfstream IV-SP (G-IV) in snowstorm

During the WSR-03 project, the NOAA G-IV will simultaneously make a number of air chemistry measurements in the upper troposphere and lower stratosphere in the active jet stream area above the Pacific winter storms. Measurements will include ozone, carbon monoxide, and volatile organic compounds, also known as hydrocarbons. Also, in the late February and early March 2003 period, the G-IV will fly coordinated missions with NASA aircraft to thoroughly profile the atmosphere directly from aircraft sensors and with dropwindsondes. NASA uses this information for validation of satellite instruments and for future satellite design.


For more information on the Winter Storms project visit http://www.emc.ncep.noaa.gov/

 

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