Hawker Siddeley Harrier

· Hawker Siddeley

Airplanes

Length

14.0208 m

Flat Wing Span

7.62 m

Height

3.3528 m

Flat Wing Area

18.6828 m²

Flat Wing Aspect Ratio

3.175

Max Speed

1176.019 km/h

Max Ceiling

15605.76 m

Number of Engines

First Flight

1967-12-28

Entry Into service

1969-04-01

Number Built

278

Maximum Take-Off Weight

11.4305 t (paragliders: kg)

Total Fuel Capacity

454.609

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity
Hawker Siddeley Harrier	11.4305	454.609

All data (27 fields)

Name: Hawker Siddeley Harrier
Manufacturer: Hawker Siddeley
Description: The Hawker Siddeley Harrier is a British jet-powered attack aircraft designed and produced by the British aerospace company Hawker Siddeley.
ICAO Code: HAR
First Flight: 1967-12-28
Entry Into service: 1969-04-01
Production End: 1986-01-01
Service End: 2006-01-01
Designer: Hawker Siddeley
Length (m): 14.0208
Height (m): 3.3528
Cockpit Crew: 1
Max Speed (km/h): 1176.019
Max Ceiling (m): 15605.76
Armament: 2× 30 mm (1.18 in) ADEN cannon pods under the fuselage; 4× under-wing & 1× under-fuselage pylon stations
Endurance (h): 1
National Origin: United Kingdom
Number Built: 278
Powerplant Description: 1 × Rolls-Royce Pegasus 103 vectored-thrust high-bypass turbofan engine
Primary Users: Royal Air Force (historical), United States Marine Corps (historical) , Spanish Navy (historical) , Royal Thai Navy (historical)
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Hawker_Siddeley_Harrier
Flat Wing Span (m): 7.62
Flat Wing Area (m²): 18.6828
Flat Wing Aspect Ratio: 3.175
Wake Category: M
Number of Engines: 1