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Hawker Siddeley / British Aerospace Harrier GR.1/GR.3

Hawker Siddeley / BAe Harrier GR.Mk.1 ex RAF © Karsten Palt
Photo ©: Karsten Palt

Harrier GR.1/GR.3

V/STOL Fighter Bomber

The Hawker Siddeley Harrier GR.1/GR.3 is a single-engine single-seat vertical/short takeoff and landing (V/STOL) fighter bomber aircraft produced by the British manufacturer Hawker Siddeley Aircraft Ltd., later BAe, British Aerospace. The Harrier was operated by the Royal Air Force (GR.1/GR.3), the Royal Thai Navy (AV-8S & TAV-8S), the Spanish Navy (AV-8S/VA-1 Matador & TAV-8S) and the United States Marine Corps (AV-8A/C & TAV-8A).

Crew1
 
Propulsion1 Turbofan Engine
Engine ModelRolls-Royce Pegasus 11 Mk.103
Engine Power95,6 kN21498 lbf
 
Speed1200 km/h648 kts
  746 mph
Service Ceiling16.764 m55.000 ft
Range648 km350 NM
403 mi.
 
Empty Weight5.579 kg12.300 lbs
max. Takeoff Weight11.340 kg25.000 lbs
 
Wing Span7,70 m25,3 ft
Wing Area18,7 m²201 ft²
Length13,87 m45,5 ft
Height3,45 m11,3 ft
 
First Flight21.10.1960
Production Statusout of production
Total Productionca. 300
 
Data for (Version)British Aerospace Harrier GR.Mk3
VariantsHarrier GR.1, GR.1A, GR.3, T.2, T.2A, T.4, T.4N, AV-8A (Mk.50), AV-8C, AV-8S / VA-1 Matador (Mk.53/55), TAV-8A (Mk.54), TAV-8S / VAE-1 Matador (Mk.54)

Remarks
The Harrier GR.1 is powered by a Rolls-Royce Pegasus 6 Mk.101 engine with a thrust of 84,5 kN (19000 lbs). The updated GR.1A is powered by a Pegasus 10 Mk.102 engine with 91,2 kN (20500 lbs) thrust. The AV-8A of the US Marine Corps is a variant of the GR.1 with the Pegasus 11 Mk.103 engine of the GR.3. The Harrier was developed into the BAe Sea Harrier and the Harrier II (GR.5, GR.7, GR.9, AV-8B).


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