The Northrop Grumman (formerly Ryan Aeronautical)
RQ-4 Global Hawk is an unmanned aerial vehicle (UAV) used by the United States
Air Force and Navy and the German Air Force as a surveillance aircraft.
In role and operational design, the Global Hawk is
similar to the Lockheed U-2, the venerable 1950s spy plane. It is a theater
commander's asset to provide a broad overview and systematic target
surveillance. For this purpose, the Global Hawk is able to provide high resolution
synthetic aperture radar (SAR) – that can penetrate cloud-cover and sandstorms
– and electro-optical/infrared (EO/IR) imagery at long range with long loiter
times over target areas. It can survey as much as 40,000 square miles (103,600
square kilometers) of terrain a day.
It is used as a high-altitude platform for
surveillance and security. Missions for the Global Hawk cover the spectrum of
intelligence collection capability to support forces in worldwide military
operations. According to the United States Air Force, the capabilities of the
aircraft allow more precise targeting of weapons and better protection of
forces through superior surveillance capabilities. The Global Hawk costs about
US$35 million to procure each aircraft. With development costs included, the
unit cost rises to US$218 million.
Design
The RQ-4 is powered by an Allison Rolls-Royce
AE3007H turbofan engine with 7,050 lbf (31.4 kN) thrust, and carries a payload
of 2,000 pounds (900 kilograms). The main fuselage is standard aluminum,
semi-monocoque construction, while the wings are made of lightweight,
high-strength composite materials.
Integrated
system
The Global Hawk UAV system comprises an air vehicle
segment consisting of air vehicles with sensor payloads, avionics, and data links;
a ground segment consisting of a Launch and Recovery Element (LRE), and a
Mission Control Element (MCE) with embedded ground communications equipment; a
support element; and trained personnel.
The Integrated Sensor Suite (ISS) is provided by
Raytheon and consists of a synthetic aperture radar (SAR), electro-optical
(EO), and infrared (IR) sensors. Either the EO or the IR sensors can operate
simultaneously with the SAR. Each of the sensors provides wide area search
imagery and a high-resolution spot mode. The SAR has a ground moving target
indicator (GMTI) mode, which can provide a text message providing the moving
target's position and velocity. Both SAR and EO/IR imagery are processed on
board the aircraft and transmitted to the MCE as individual frames. The MCE can
mosaic these frames into images prior to further dissemination.
Navigation is via inertial navigation with
integrated Global Positioning System updates. Global Hawk is intended to
operate autonomously and "untethered" using a satellite data link
(either Ku or UHF) for sending sensor data from the aircraft to the MCE. The
common data link can also be used for direct down link of imagery when the UAV
is operating within line-of-sight of users with compatible ground stations.
The ground segment consists of a Mission Control
Element (MCE) and Launch and Recovery Element (LRE), provided by Raytheon. The
MCE is used for mission planning, command and control, and image processing and
dissemination; an LRE for controlling launch and recovery; and associated
ground support equipment. (The LRE provides precision differential global
positioning system corrections for navigational accuracy during takeoff and
landings, while precision coded GPS supplemented with an inertial navigation
system is used during mission execution.) By having separable elements in the
ground segment, the MCE and the LRE can operate in geographically separate
locations, and the MCE can be deployed with the supported command's primary
exploitation site. Both ground segments are contained in military shelters with
external antennas for line-of-sight and satellite communications with the air
vehicles.
Sensor
packages
The Global Hawk carries the Hughes Integrated
Surveillance & Reconnaissance (HISAR) sensor system. HISAR is a lower-cost derivative
of the ASARS-2 package that Hughes developed for the Lockheed U-2. HISAR is
also fitted in the US Army's RC-7B Airborne Reconnaissance Low Multifunction
(ARLM) manned surveillance aircraft, and is being sold on the international
market. HISAR integrates a SAR-MTI system, along with an optical and an
infrared imager. All three sensors are controlled and their outputs filtered by
a common processor. The digital sensor data can be transmitted at up to 50
Mbit/s to a ground station in real time, either directly or through a
communications satellite link.
The SAR-MTI system operates in the X-band and
provides a number of operational modes:
The wide-area MTI mode can detect moving targets
within a radius of 62 miles (100 kilometers).
The combined SAR-MTI strip mode provides 20 foot (6
meter) resolution over a swath 23 miles (37 kilometers) wide at ranges from
12.4 to 68 miles (20 to 110 kilometers).
The SAR spot mode can provide 6 foot (1.8 meter)
resolution over 3.8 square miles (10 square kilometers), as well as provide a
sea-surveillance function.
The visible and infrared imagers share the same
gimballed sensor package, and use common optics, providing a telescopic
close-up capability. It can be optionally fitted with an auxiliary SIGINT
package. To improve survivability, the Global Hawk is fitted with a Raytheon
developed AN/ALR-89 self-protection suite consisting of the AN/AVR-3 Laser
Warning System, AN/APR-49 Radar Warning Receiver and a jamming system. An
ALE-50 towed decoy also aids in the Global Hawk's deception of enemy air
defenses.
In July 2006, the US Air Force began testing
segments of the improved Global Hawk Block 30 upgrades in the Benefield
Anechoic Facility at Edwards AFB. This version incorporates an extremely
sensitive SIGINT processor known as the Advanced Signals Intelligence Payload.
In September 2006, testing began on a new specialty
radar system, the Multi-Platform Radar Technology Insertion Program, or
MP-RTIP, on board the Scaled Composites Proteus. Once validated, one Global
Hawk will be modified to carry this radar set. Previously, the Air Force was
considering a larger variant of the MP-RTIP (known as the Wide-Area
Surveillance or WAS sensor) for the canceled E-10 MC2A testbed or E-8 Joint
STARS aircraft.
In August 2010, Northrop announced that a new
version, Block 40, was about to commence production; it would have a new sensor
capabilities, including MP-RTIP radar, emphasising surveillance over
reconnaissance. The Block 40 design also has a modified undercarriage.
Specifications
RQ-4A
General characteristics
Crew
|
0
|
Length
|
44 ft 5 in (13.54 m)
|
Wingspan
|
116 ft 2 in (35.41 m)
|
Height
|
15 ft 2 in (4.62 m)
|
Empty weight
|
8,490 lb (3,851 kg)
|
Gross weight
|
22,900 lb (10,387 kg)
|
Powerplant
|
1 × Allison Rolls-Royce AE3007H
turbofan engine, 7,050 lbf (31.4 kN) thrust
|
Performance
Maximum speed
|
497.1 mph (800 km/h; 432 kn)
|
Cruise speed
|
404 mph (351 kn; 650 km/h)
|
Range
|
15,525 mi (13,491 nmi; 24,985 km)
|
Endurance
|
36 hours
|
Service ceiling
|
65,000 ft (19,812 m)
|
RQ-4B
General characteristics
Crew
|
0 onboard (3 remote: LRE pilot; MCE
pilot and sensor operator)
|
Length
|
47.6 ft (14.5 m)
|
Wingspan
|
130.9 ft (39.9 m)
|
Height
|
15.3 ft (4.7 m)
|
Empty weight
|
14,950 lb (6,781 kg)
|
Gross weight
|
32,250 lb (14,628 kg)
|
Powerplant
|
1 × Allison Rolls-Royce F137-RR-100
turbofan engine, 7,600 lbf (34 kN) thrust
|
Performance
Cruise speed
|
357 mph (310 kn; 575 km/h)
|
Range
|
8,700 mi (7,560 nmi; 14,001 km)
|
Endurance
|
28 hours
|
Service ceiling
|
60,000 ft (18,288 m)
|
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