The Global Hawk air vehicles are built at the Northrop
Grumman (formerly Teledyne Ryan) aeronautical facility in San Diego.
Northrop Grumman Corporation, Ryan Aeronautical Centre is the
prime contractor and the principal suppliers include Raytheon Systems
(sensors), Rolls-Royce North America (turbofan engine), Boeing North American
(carbon fibre wing) and L3 Communications (communications system). The
programme is funded by the Defense Airborne Reconnaissance Office (DARO) and
managed by the Defense Advanced Research Projects Agency (DARPA) and the US Air
Force.
RQ-4A Global Hawk is a high-altitude, long-endurance unmanned
aerial reconnaissance system which provides military field commanders with high
resolution, near real-time imagery of large geographic areas.
Development
In March 2001, the US Department of Defense awarded Northrop
Grumman a contract for the Engineering and Manufacturing Development (EMD)
phase of the programme which concluded in February 2003 with the final delivery
of the seventh pre-production (block 0) vehicle.
In June 2001 a contract was
placed to begin low-rate initial production (LRIP) for two production air
vehicles and the mission control element of the system's ground station, to be
completed by December 2003.
The first production vehicle
(block 10) rolled out in August 2003. A further LRIP contract for four vehicles
was placed in February 2003 and a third in October 2004 for two vehicles. Block
10 deliveries were completed in June 2006.
The US Navy had two RQ-4A air
vehicles delivered in 2005. In April 2008, the USN selected the RQ-4N marinised
variant of the Global Hawk RQ-4B Block 20 for the broad-area maritime
surveillance (BAMS) unmanned aircraft system (UAS) requirement.
The system design and
development (SDD) contract awarded to Northrop Grumman requires the delivery of
two UAVs with mission payloads and communication suites, one forward operating
base mission control system, one systems integration laboratory and one main
operating base mission control system.
The RQ-4N will have a Northrop
Grumman active electronically scanned array (AESA) radar, Raytheon
electro-optic / infrared sensors, L-3 communications suite and Sierra Nevada
Corp. Merlin electronic support measures (ESM). The RQ-4N is planned for
service entry in 2014.
RQ-4B Next
Generation Reconnaissance Drone
Northrop Grumman is developing
the next-generation, RQ-4B, which has a 50% payload increase, larger wingspan
(130.9ft) and longer fuselage (47.6ft), and new generator to provide 150% more
electrical output. Three RQ-4B air vehicles (block 20) were initially ordered
plus a further five ordered in November 2005. Block 20 aircraft also have an
upgraded sensor suite.
The first block 20 Global Hawk
completed a maiden flight in April 2007 and the first was delivered in June
2008. 26 block 30 with a signals intelligence (SIGINT) payload will be ordered
and 15 block 40 with the multi-platform radar technology insertion programme
(MP-RTIP) radar, to enter service from 2011. The US Air Force plans a total of
54 air vehicles.
The block 40 Global Hawk, with the multi-platform radar
technology insertion programme (MP-RTIP), has been selected by Nato for the
alliance ground surveillance (AGS) programme. The original proposal had manned
and unmanned elements but the Alliance decided to go ahead with a UAV-only
programme in September 2007. Northrop Grumman will be the prime contractor.
The Australian Defence Force
has plans to purchase a squadron of Global Hawks to replace a number of P-3C
Orion maritime patrol aircraft.
Global
Hawk's Record-breaking Flights
In April 2001, Global Hawk made
aviation history when it completed the first non-stop flight across the Pacific
Ocean by an unmanned, powered aircraft, flying from Edwards AFB, California, to
the Royal Australian Air Force Base, Edinburgh, South Australia.
Global Hawk successfully
participated in a series of exercises with the RAAF, the Royal Australian Navy
and the US Navy. Guinness World Records has recognised the flight as the
longest (13,840km) by a full-scale unmanned aircraft.
In August 2003, Global Hawk
became the first UAV to receive authorisation from the US Federal Aviation
Administration (FAA) to fly in national airspace.
Unmanned Reconnaissance Capability
Global Hawk can carry out
reconnaissance missions in all types of operations. The 14,000nm range and
42-hour endurance of the air vehicle, combined with satellite and line-of-sight
communication links to ground forces, permits worldwide operation of the system.
High-resolution sensors,
including visible and infrared electro-optical systems and synthetic aperture
radar, will conduct surveillance over an area of 40,000nm² to an altitude of
65,000ft in 24 hours.
Six Global Hawk demonstrator
vehicles have been deployed in support of Operation Enduring Freedom in
Afghanistan since 2002 and Operation Iraqi Freedom since 2003, completing over
4,300 combat hours.
Two ex-USAF Global Hawk
demonstrators were transferred to NASA's Dryden Research Center at Edwards AFB,
California in January 2008, for use as airborne science research platforms.
Flight
and Navigation Control
The vehicle's flight control,
vehicle management software and navigation functions are managed by two
integrated mission management computers (IMMC) developed by Vista Controls
Corporation, California. The IMMC integrates data from the navigation system and
uses Kalman filtering algorithms.
The prime navigation and
control system consists of two KN-4072 INS/GPS (inertial navigation system /
global positioning system) systems supplied by Kearfott Guidance &
Navigation Corporation of Wayne, New Jersey.
The KN-4072 includes a monolithic ring laser gyro (MRLG)
which operates in conjunction with an embedded differential ready C/A code GPS
receiver for enhanced navigation performance and faster satellite acquisition.
A Northrop Grumman (Litton) navigation system is installed on the IR/TV/SAR
payload.
Sensors
Raytheon Space & Airborne
Systems supplies the Global Hawk integrated sensor suite (ISS) which includes
the synthetic aperture radar and the electro-optical and third-generation
infrared sensor system.
A 10in reflecting telescope
provides common optics for infrared and electro-optical sensors. The
electro-optical / infrared sensor operates in the 0.4 to 0.8 micron visible
waveband and the 3.6 to 5-micron infrared band. In spot collection mode the
coverage is 1,900 spots a day with spot size 2km² to a geological accuracy of
20m circular error of probability. In wide area search mode, the swath is 10km
wide and the coverage is 40,000nm² a day.
The synthetic aperture radar
and ground moving target indicator (GMTI) operates at X-band with a 600MHz
bandwidth, and 3.5kW peak power. The system can obtain images with 3ft
resolution in its wide area search mode and 1ft resolution in its spot mode.
Raytheon is contracted to
supply one enhanced integrated sensor suite (EISS) which is said to improve the
range of both SAR and infrared system by 50%.
The Raytheon ground station
receives the high-quality imagery obtained by the air vehicle sensor suite. The
ground system forwards the imagery to military commanders and users in the
field.
Northrop Grumman is prime
contractor, with Raytheon as major subcontractor, for the USAF multi-platform
radar technology insertion program (MP-RTIP). MP-RTIP is an active
electronically scanned array (AESA) radar that can be scaled in size for different
platforms.
Three MP-RTIP systems are being
built for Global Hawk and three for the E-10A multi-sensor command and control
aircraft (MC2A).
In January 2006, a Global Hawk made its first flight carrying
Northrop Grumman's high-band system production configuration unit (HBS PCU),
part of the USAF's airborne signals intelligence payload. Northrop Grumman is
also looking at other payloads including hyperspectral sensors for chemical and
biological agent detection.
In November 2003, Global Hawk
completed a series of flight tests in the USA and Germany carrying an EADS
electronic intelligence (ELINT) payload. The 'Euro Hawk' is being offered to
the German Air Force as a replacement SIGINT platform.
In February 2007, the German
Air Force awarded a contract to Eurohawk GmbH (a joint venture company formed
by Northrop Grumman and EADS) for the development of Euro Hawk.
Communications
Global Hawk has wide band
satellite data links and line of sight data links developed by L3
Communications. The 'bulge' at the top front surface of the fuselage which
gives Global Hawk its distinctive appearance, houses the 48in Ku-band wideband
satellite communications antenna. Data is transferred by Ku-band satellite
communications, X-band line-of-sight links and both Satcom and line of sight
links at UHF-band.
Survivability
For increased survivability the
mission is planned for threat avoidance using available theatre assets such as
AWACS, combat air patrol and JSTARS. The aircraft flies high at a loiter
altitude 65,000ft which minimises exposure to surface-to-air missiles. The
aircraft's modular self-defence system includes an AN/ALR 89 radar warning
receiver, an on-board jamming system and an ALE 50 towed decoy system.
Air Vehicle Construction
The wings and tail of the
aircraft are of graphite composite construction. The V-configuration of the
tail, built by Aurora Flight Sciences, provides a low radar and infrared
signature. The wings, constructed by Vought Aircraft Industries, have a span of
116.2ft, with hard points for external pods up to 1,000lb each. Vought and ATK
are fabricating an enhanced wing, one of a number of system improvements to
enable Global Hawk to carry an increased payload.
The aluminium fuselage contains
pressurised payload and avionics compartments. Honeywell Aerospace, Torrance,
California, supplied the environmental control systems.
The landing gear is supplied by Heroux Inc. of Quebec, Canada.
The nose gear which is a derivative of the F-5 design is height adjustable to
suit the runway characteristics. The landing gear automatically retracts at an
altitude of 4,000ft.
Global Hawk is equipped with an
AE 3007H turbofan engine supplied by Rolls-Royce North America. The engine is
mounted on the top surface of the rear fuselage section with the engine exhaust
between the V-shaped tail wings. Smiths Aerospace is providing a new electric generator
system to more than double electrical power.
Mission
Planning
Mission planning for the Global
Hawk was developed by GDE Systems Inc (now BAE Systems, Electronics &
Integrated Solutions). The Raytheon Intelligence & Information Systems
mission control ground station includes a shelter measuring 8ft×8ft×24ft
housing the communications, command and control, mission planning and image
processing computers with four workstations for the mission control staff and
officers. The mission control centre has data up- and down-links to the Global
Hawk vehicle directly and via the Ku satellite and the UHF satellite systems.
The Raytheon launch and
recovery ground station is housed in an 8ft x 8ft x 10ft shelter equipped with
two workstations and the launch and recovery mission computers. The launch and
recovery station has up- and down- data communications links to the Global Hawk
vehicle and to the UHF communications satellite.
Transportability
The complete mission control
element (MCE) and the launch and recovery element (LRE) is transportable in a
single load on the C-5B transporter aircraft and in less than two loads on the
C-17 transporter.
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