The British Aerospace Harrier II is the second-generation Harrier vertical and short takeoff jet that the Royal Air Force flew as the GR5, GR7 and GR9, and that the Royal Navy also flew from 2006 to 2010. It was an Anglicised version of the McDonnell Douglas AV-8B, built with British Aerospace as prime contractor and McDonnell Douglas as sub-contractor, with final assembly at Dunsfold in England. The first British-built development aircraft flew on 30 April 1985. The GR5 was upgraded to the GR7 with night attack avionics, and later aircraft were brought to GR9 standard with a metal rear fuselage and further avionics updates. The type served in Kosovo, Iraq and Afghanistan, mainly in air interdiction and close air support, and was retired early in December 2010 after the Strategic Defence and Security Review. This entry covers the British Aerospace aircraft; the American-built AV-8B is a separate entry.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) EngineRolls-Royce Pegasus Mk. 105 turbofan 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Derived From
Source British Aerospace Harrier II (Wikipedia)
Exemplifies
Source British Aerospace Harrier II (Wikipedia)
Of Make
Source British Aerospace Harrier II (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source British Aerospace Harrier II (Wikipedia)Design and development, Origins, manufacturerQuote, Design and development, Origins, manufacturer
British Aerospace producing the aircraft as the prime contractor, with McDonnell Douglas serving as a sub-contractor
Originated In
Also in Geography Atlas: where this subject originated.
Source British Aerospace Harrier II (Wikipedia)Design and development, final assemblyQuote, Design and development, final assembly
final assembly work was performed at Dunsfold, England
Sources
1. British Aerospace Harrier II (Wikipedia)
Design and development, Origins
first BAe-built development GR5 flew for the first time on 30 April 1985
Lead
is a second-generation vertical/short takeoff and landing (V/STOL) jet aircraft
Lead, retirement
In December 2010, budgetary pressures led to the early retirement of all Harrier IIs from service
Specifications (Harrier GR7), empty weight
Empty weight: 12,500 lb (5,670 kg)
Specifications (Harrier GR7), take-off weight
Max takeoff weight: 31,000 lb (14,061 kg) STO
Specifications (Harrier GR7), speed
Maximum speed: 575 kn (662 mph, 1,065 km/h)
Specifications (Harrier GR7), powerplant
1 × Rolls-Royce Pegasus Mk. 105 turbofan engine
Design and development, Origins, manufacturer
British Aerospace producing the aircraft as the prime contractor, with McDonnell Douglas serving as a sub-contractor
Design and development, final assembly
final assembly work was performed at Dunsfold, England
In Group: Ground-Attack and Dive Bombers, Lead, role
The type's main function was as a platform for air interdiction and close air support missions
Derived From: McDonnell Douglas AV-8B Harrier II, Lead, derivation
was derived from the McDonnell Douglas AV-8B Harrier II
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