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Read the entry →Hawker Siddeley
The Harrier was a British V/STOL multi-role military aircraft. It is a single-seat, single-engine jet fighter with the ability to land vertically, like a helicopter. The aircraft was designed and built by British aerospace company Hawker Siddeley (now part of British Aerospace). The Royal Air Force (RAF) first deployed the aircraft in 1969. Later in its career the aircraft was also used for air-to-air combat and air patrol as well as maritime surveillance.
In 1969, the RAF Harrier entered Royal Air Force service as the first jet aircraft capable of vertical takeoff and landing. Developed by Hawker Siddeley and powered by the Rolls-Royce Pegasus engine, it represented a clear break from the long-runway model that had dominated jet operations since the Second World War. In the tense Cold War environment, this capability was more than a technical milestone; it answered a pressing strategic concern about the survivability of air power in the opening hours of a major conflict.
NATO planners expected that any large-scale war in Europe would begin with heavy attacks on fixed air bases. Conventional fighters, tied to long, prepared runways, would be vulnerable on the ground. The Harrier concept was conceived as a direct response to this problem. Operating from short strips of road, forest clearings, or simple temporary pads, it enabled combat aircraft to remain dispersed and harder to target.
The core of this innovation lay in the vectored-thrust Pegasus engine, which allowed the RAF Harrier to lift vertically, hover, and then accelerate into normal forward flight. This flexibility in how and where it could operate altered thinking about close air support, forward basing, and expeditionary warfare. The aircraft demonstrated that a frontline jet could operate without the traditional infrastructure that had previously been taken for granted.
The RAF Harrier grew out of late 1950s concern that major airfields in Europe would be prime targets in any nuclear or conventional exchange. Air Staff planning began to favour aircraft that could operate from dispersed sites, close to the front line and away from obvious targets. This requirement led the RAF and British industry to explore vertical take-off and landing concepts that could give a modern jet fighter the same basing freedom as a helicopter, but with the speed and striking power of a fast jet.
The Harrier programme was an attempt to translate that concept into a practical front-line system.
The key step was the Hawker P.1127, which first flew in October 1960. This prototype used the Pegasus engine, whose four swivelling exhaust nozzles could direct thrust downward for lift or rearward for forward flight. In vertical mode, the aircraft rose straight up under jet thrust; as it gained height, the pilot could slowly rotate the nozzles rearwards, allowing the wings to take over and the aircraft to accelerate into normal flight. This basic method, later refined, would define how every RAF Harrier flew for the rest of its career.
In operational terms, vectored thrust meant a pilot could lift vertically or with a very short ground roll using downward-directed jet thrust. By rotating the nozzles, lift could be shared between the engine and the wings, allowing a smooth transition into conventional forward flight once the wings were fully supporting the aircraft.
The P.1127 led to the Kestrel FGA.1 evaluation aircraft, tested by a joint group of British, American, and West German pilots under the Tripartite Evaluation Squadron in 1964–65. These trials confirmed that vectored thrust could be used safely in day-to-day operations, not just in controlled test conditions. On this foundation, Hawker Siddeley developed the first production RAF Harrier, the Harrier GR.1, which entered service with No. 1 Squadron in April 1969 as a dedicated ground-attack and close-air-support aircraft.
Short take-off techniques soon became central to operations. By using a brief forward run before rotating the nozzles, the RAF Harrier could combine jet thrust with wing lift and leave the ground with much more fuel and weapons than a pure vertical launch allowed. This method, and later the use of ski-jump ramps at sea, balanced the aircraft’s vertical capability with practical combat loads and realistic sortie rates.
Early experience identified useful improvements, which appeared in the Harrier GR.3, which entered service in the mid-1970s. The GR.3 carried a more powerful Pegasus engine and a revised avionics fit. It also gained a distinctive extended nose housing the Ferranti Laser Ranger and Marked Target Seeker (LRMTS), enabling more accurate weapon delivery. Additional defensive equipment increased survivability in dense air defence environments, turning the GR.3 into a more mature and capable VTOL strike platform.
The RAF Harrier was not only a technical innovation; it sat at the centre of a distinct operational doctrine. In Central Europe, RAF squadrons were planned to disperse away from established bases as soon as war seemed likely. Instead of broad, obvious runways, the RAF Harrier would fly from simple forward sites, often pre-surveyed stretches of road or small clearings that could be adapted for aviation use with minimal preparation.
Typical Harrier operating locations included short, straight sections of public highway surveyed in peacetime, small grass or concrete strips near woodland or villages, and temporary metal-planked pads laid in open fields or clearings.
At these locations, aircraft would be parked in camouflaged hides, screened from view and arranged to reduce the risk that a single attack could destroy several machines at once. Mobile support teams moved with the Harrier force, bringing fuel, weapons, and basic maintenance equipment on lorries and trailers. Refuelling and re-arming took place at the edge of woodland or beside minor roads rather than on large dispersals. This approach accepted a more austere working environment in exchange for a smaller and less predictable target footprint.
The primary task in this setting was close air support and interdiction against advancing armoured formations. The RAF Harrier was intended to strike tanks, artillery, and supply lines at short notice, flying from sites relatively close to the front while remaining difficult to locate. Its ability to operate from short sections of roadway meant that if one site was compromised, aircraft and support crews could move quickly to another, preserving combat power even under heavy attack.
This doctrine was not confined to Central Europe. RAF Harrier units also deployed to Norway for cold-weather exercises, practising operations from austere northern locations with limited permanent infrastructure. In Belize, the aircraft provided a visible and responsive presence, again using short or basic strips. In each case, the RAF Harrier demonstrated the same core idea: a fast jet that could continue to fight even if conventional bases were damaged or unavailable.
The RAF Harrier’s most famous test came during the Falklands War of 1982. When Argentine forces occupied the islands, British planners faced the challenge of conducting air operations at a great distance from the United Kingdom and without friendly mainland bases in the region. Carrier air power became the only practical means of gaining local air superiority and providing close support for land forces once they went ashore. In this setting, the Harrier’s short take-off and vertical landing qualities took on particular importance.
A detachment of RAF Harrier GR.3 aircraft embarked in HMS Hermes and later operated alongside Royal Navy Sea Harriers. The GR.3s, optimised for ground attack, were adapted for maritime operations and integrated into the wider air group. From the carrier, the RAF Harrier launched repeated sorties against Argentine positions on the islands, striking radar sites, artillery, and logistic targets. These missions supported both the naval effort and the land campaign, often at low level and in demanding weather conditions.
The South Atlantic environment was challenging, with strong winds, low cloud, and sea states that tested both ships and aircraft. In these conditions, the RAF Harrier showed its value. The ability to approach slowly and use nozzle control enabled pilots to achieve fine handling during deck landings. The aircraft also proved robust in a maritime environment, an important test for a land-based strike jet.
As British land forces advanced, engineers laid a forward operating strip at San Carlos using metal matting. RAF Harrier GR.3s then operated from this temporary site, reducing transit times and increasing sortie rates in support of ground forces. The performance of both RAF and Royal Navy Harriers in the Falklands confirmed the operational practicality of the concept under combat conditions.
The aircraft’s combat record continued after 1982. During the 1991 Gulf War, later-generation RAF Harriers flew strike and reconnaissance missions against Iraqi forces. In subsequent operations over the Balkans in the 1990s, and later in Afghanistan during the 2000s, RAF Harrier variants again provided close air support to ground troops. Across these conflicts, the Harrier family demonstrated flexibility and combat effectiveness in environments that often lacked extensive aviation infrastructure.
These campaigns showed that a concept first conceived for Cold War Europe could be adapted to very different climates, terrains, and types of conflict while retaining its central advantages.
| Dimensions | |
| Wingspan | 25 ft 5 in (7.75 m) |
| Length | 46 ft 10 in (14.27 m) |
| Height | 11 ft 11 in (3.63 m) |
| Wing area | 201.1 sq ft (18.68 m²) |
| Weights | |
| Empty weight | 13,535 lb (6,139 kg) |
| Max takeoff weight | 25,200 lb (11,431 kg) |
| Max bomb load | 5,000 lb (2,268 kg) |
| Performance | |
| Maximum speed | 731 mph (1,176 km/h) |
| Cruise speed | 500 mph (805 km/h) |
| Service ceiling | 51,200 ft (15,600 m) |
| Range | 2,130 mi (3,430 km) |
| Powerplant | |
| Engines | 1 × Rolls-Royce Pegasus 103 vectored-thrust turbofan |
| Power | 21,500 lbf (96 kN) thrust with water injection |
| Armament | |
| Guns | 2 × 30 mm ADEN cannon pods with provision for up to 5,000 lb (2,268 kg) of bombs, rockets, BL755 cluster bombs and AIM-9 Sidewinders |
| Bombs / weapons | 5,000 lb (2,268 kg) |
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