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British Aerospace Harrier II

Military Aircraft

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
Year
1985 1
Engine Class
Jet 1
Status
Retired from service 1
Top Speed (km/h)
1065 1
Mass (kg)
5670 1
Maximum Mass (kg)
14,061 1
Engine
Rolls-Royce Pegasus Mk. 105 turbofan 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Derived From

Source British Aerospace Harrier II (Wikipedia)

Exemplifies

Aviation, Modes
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, manufacturer
Quote, 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 assembly
Quote, 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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