British Aerospace Harrier II

British Aerospace Harrier II
Zemlja	Velike britanije
Ulogu	V/STOL udarna letelica
Prvi let	30 April 1985
Izgradio	143

Čaj British Aerospace Harrier II je avion druge generacije vertikalno/kratko poletanje i sletanje (V/STOL) koji je prethodno koristilo Kraljevsko vazduhoplovstvo (RAF) i, između 2006. Letelica je bila najnoviji razvoj porodice Harrier Jump Jet, a izvedena je iz mcDonnell Douglas AV-8B Harrier II. Inicijalne isporuke HarrierA II označene su u službi kao Harrier GR5; naknadno modernizovani avioni su redizajnirani u skladu sa tim kao GR7 i GR9.

Izvor: British Aerospace Harrier II on Wikipedia

BAe Harrier GR.9 Walk Around
Photographer	Vladimir Yakubov
Localisation	Imperial War Museum, London
Photos	149

British Aerospace Harrier GR.9 01

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British Aerospace Harrier GR.9 07

British Aerospace Harrier GR.9 08

British Aerospace Harrier GR.9 09

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Harrier GR.7 Walk Around
Fotograf	Burhand Donke
Lokalizacija	Nepoznato
Fotografije	28

Harrier GR.7 01

Harrier GR.7 02

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Harrier GR.7 06

Harrier GR.7 07

Harrier GR.7 08

Harrier GR.7 09

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General Characteristics and Role

The British Aerospace Harrier GR.9 was a major upgrade of the earlier GR.7 model, serving as the final ground-attack/reconnaissance variant of the **second-generation Harrier II family** (a development of the original Hawker Siddeley Harrier). The GR.9 was specifically designed for Vertical/Short Take-Off and Landing (V/STOL) operations, allowing it to operate from small clearings, roads, or the decks of aircraft carriers without a catapult. Its primary role was close air support (CAS) and battlefield interdiction. The upgrade focused on improved avionics, greater precision strike capability (including the integration of modern smart weapons), and a more powerful engine to cope with increased weapon loads. The Harrier GR.9 served with the Royal Air Force (RAF) and the Royal Navy (RN) until the type’s retirement in 2010.

Property	Typical Value (Harrier GR.9)
Ulogu	V/STOL Ground Attack, Reconnaissance
National Origin	United Kingdom / United States (Joint Development)
Proizvođača	British Aerospace / McDonnell Douglas
Service Entry (GR.9)	2006
Posada	1 (Pilot)
Dužina	14.12 m (46 ft 4 in)
Raspon krila	9.25 m (30 ft 4 in)
Visina	3.56 m (11 ft 8 in)
Max Takeoff Weight (STOVL)	14,000 kg (31,000 lb)

Powerplant and V/STOL System

Engine: 1 x Rolls-Royce Pegasus Mk. 107 vectored-thrust turbofan.
Max Thrust: Approximately 105.87 kN (23,800 lbf).
Maximum Speed: 1,065 km/h (662 mph; 575 kn) (Mach 0.87) at sea level.
Operational Range: Approximately 3,300 km (2,000 mi) with external fuel tanks.
V/STOL Principle: Thrust is directed through four rotating nozzles (two hot exhaust, two cold bypass air) located around the aircraft’s center of gravity. This allows the thrust to be directed downward for vertical flight or rearward for horizontal flight.

Armament and Avionics

Hardpoints: 7 external stations for weapons and fuel.
Primary Armament: Often included Paveway II/III laser-guided bombs, Enhanced Paveway II/III GPS-guided bombs, AGM-65 Maverick air-to-ground missiles, and CRV7 rocket pods.
Avionics: Upgraded navigation and weapon systems, including the integration of GPS/INS for all-weather precision attack and a new digital cockpit architecture.
Self-Defense: Equipped with defensive aids systems (DAS) including radar warning receivers and chaff/flare dispensers.

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