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The Harrier GR5, GR7, GR7A, GR9 and GR9A are all Royal Air Force variants of the BAE Systems / Boeing Harrier II .

The Aircraft was solely designed and built by British Aerospace, However the US have their own license built varients of inferior performance. For UK variants BAE Systems is the prime contractor and Boeing sub-contractor. The USAF currently has no equivalent of the British Harrier II Plus Night Attack.

The Harrier II is an extensively modified version of the first generation Hawker-Siddeley Harrier GR Mk.1/Mk.3 series which first flew in December, 1967. The original aluminium alloy fuselage was replaced by a fuselage which makes extensive use of composites, providing significant weight reduction, increased payload/range. A totally new one piece wing provides around 14 per cent more area and increased thickness.

Unlike the Harrier AV8B + upgrade the RAF have chosen not to integrate a radar into its aircraft. This is because the Harrier has an Integrated Inertial Navigation System that is extremely accurate. The primary Air-to-air Missile (AAM) of the Harrier is the AIM-9 Sidewinder using its infrared homing device, the harrier/sidewinder cocktail proved a lethal one to the Argentinian Mirages in the Falklands conflict. With the retirement of the Sea Harrier it has been suggested that its Blue Vixen radar could be transferred to the GR9 fleet however the Ministry Of Defence has rejected this as risky and too expensive, Defence Minister Adam Ingram estimated the cost would be in excess of £600m.


VARIANTS


GR5

The GR5 was the RAF's first 2nd generation Harrier with development beginning in 1976. Two AV-8As were modified to Harrier II standard in 1979 and operated as development aircraft. The first BAe built development GR5 flew for the first time on April 30 , 1985 and the aircraft entered service in July 1987. The GR5 differed from the USMC AV-8B in many subtle ways, for example avionics fit, weapons and countermeasures. Forty one GR5s were built.


GR5A

The GR5A was a minor variant of the Harrier which incorporated changes in the design in anticipation of the GR7 upgrade. Twenty one GR5As were built.


GR7

The GR7 had its maiden flight in May 1990 and made its first operational deployment in August 1995 over the former Yugoslavia . While the GR7 deployed on Invincible Class Aircraft Carrier s during testing as early as June 1994, the first operational deployments at sea began in 1997. This arrangement was formalised with the Joint Force Harrier , operating with the Royal Navy's Sea Harrier .

The GR7 formed the spearhead of the RAF's contribution to Operation Allied Force , the NATO mission in Kosovo . During this campaign the RAF identified significant shortcomings in its current arsenal. As a result the service ordered the AGM-65 Maverick stand off missile and the Enhanced Paveway which incorporates GPS guidance which would negate the effects of smoke and bad weather. Using the more updated ordnance as well as unguided iron and cluster munitions, RAF GR7's played a prominent role in Operation Telic , the UK contribution to the U.S.-led war against Iraq in 2003. RAF GR7's participated in strike and close air support missions throughout the conflict.


GR7A


2005]]

The GR7A is the first stage in an upgrade to the Harrier GR9 standard. The GR7A is the GR7 with an uprated Rolls-Royce Pegasus 107 engine. When upgraded to GR9 standard the uprated engine variants will retain the A designation, becoming GR9As. Forty GR7s are due to receive this upgrade. The Mk 107 engine provides around 3,000 lbf (13 kN) extra thrust than the Mk 105's 21,750 lbf (98 kN) thrust, increasing aircraft performance during "hot and high" and carrier borne operations.


GR9

The Harrier GR9 is an avionics and weapons upgrade of the standard GR7. This upgrade, known as the Integrated Weapons programme (IWP), allows the carriage of the latest smart weapons, new inertial navigation and Global Positioning systems ( INS / GPS ). The new weapons being integrated are the Brimstone , Maverick and Storm Shadow missiles.


GR9A

The Harrier GR9A is an avionics and weapons upgrade of the uprated engined GR7As.


T10

The Harrier T10 is the original two seat training variant of the second generation RAF Harrier. The RAF considered upgrading the 1st generation Harrier trainer, the T4, to Harrier II standard. However due to the age of the airframes and the level of modification required the service decided to order new build Harrier II trainers. The RAF used the USMC trainer, the TAV-8B, as the basis for the design. Unlike their American counterparts the T10s are fully combat capable. Thirteen aircraft were built.


T12

With the upgrades applied to the GR7s to GR9 standard the RAF requires representative trainers. These aircraft will be the T12, the T10s with the IWS upgrade.


UNITS USING THE HARRIER II


Royal Air Force




Field Reports



FUTURE

With the withdrawal of the Royal Navy's Sea Harrier by 2006 the RAF's Harrier fleet will be tasked with the missions it currently shares with those aircraft. In 2006 , the GR9 will also enter service with the Fleet Air Arm when the first former Sea Harrier squadron is reformed. The GR9 is expected to stay in service at least until 2015, when the first F-35 s are due. At this point the JSF force should be gaining an initial operational capability (IOC).


SPECIFICATIONS (HARRIER GR.7)


  plane Or Copter plane
  jet Or Prop jet
  crew 1 or 2
  length Main 46 ft 4 in
  length Alt 141 m
  span Main 30 ft 4 in
  span Alt 92 m
  height Main 11 ft 9 in
  height Alt 35 m
  area Main ft&sup2
  area Alt m&sup2
  empty Weight Main 12,500 lb
  empty Weight Alt 5,700 kg
  loaded Weight Main lb
  loaded Weight Alt kg
  max Takeoff Weight Main lb
  max Takeoff Weight Alt kg
  engine (jet) Rolls-Royce Pegasus 105
  type Of Jet Turbofan with four thrust vectored exhaust nozzles
  number Of Jets 1
  thrust Main 35,000 lb
  thrust Alt kN
  max Speed Main mach 1
  max Speed Alt 1,065 km/h
  range Main mi
  range Alt km
  ceiling Main 50,000 ft
  ceiling Alt 15,000 m
  climb Rate Main 40,000ft/min
  climb Rate Alt m/s
  loading Main lb/ft&sup2
  loading Alt kg/m&sup2
  thrust/weight VHigh



REFERENCES