BAE Systems Hawk

Airplanes

Length

12.192 m

Flat Wing Span

9.7536 m

Height

3.9624 m

Max Speed

1028 km/h

Max Ceiling

13563.6 m

Number of Engines

Aircraft Engine

First Flight

1974-08-21

Entry Into service

1976-01-01

Number Built

1000

Maximum Take-Off Weight

9.0718 t (paragliders: kg)

Maximum Range

2518.72 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
BAE Systems Hawk	9.0718	2518.72

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Sukhoi S-54		12.3	9.8	Compare
Grumman F-9 Cougar		12.192	10.3632	Compare
Royal Aircraft Factory F.E.1	De Havilland Iris	12.192	10.0584	Compare
Aero L-159 ALCA		12.72	9.54	Compare
A Vlaicu I	Gnome Omega	12	10	Compare
Farman III		12	10	Compare

All data (25 fields)

Name: BAE Systems Hawk
Manufacturer: BAE Systems
Description: The BAE Systems Hawk is a British single-engine, subsonic, jet-powered advanced trainer aircraft.
ICAO Code: HAWK
First Flight: 1974-08-21
Entry Into service: 1976-01-01
Designer: BAE Systems
Type: Advanced trainer aircraft
Length (m): 12.192
Height (m): 3.9624
Cockpit Crew: 2
Max Speed (km/h): 1028
Max Ceiling (m): 13563.6
Rate of Climb (m/s): 47.244
Armament: :Note: all armament is optional.; 1× 30 mm ADEN cannon, in centreline pod; Up to 6,800 lb (3,085 kg) of weapons on five hardpoints, including:; 4× AIM-9 Sidewinder or ASRAAM or A-Darter on wing pylons and wingtip rails; 2x Umbani or Al Tariq; Smart Anti-Airfield Weapon; 1,500 lb (680 kg), limited to one centreline and two wing pylons (Hawk T1)
National Origin: United Kingdom
Number Built: 1000
Powerplant Description: 1 × Rolls-Royce Turbomeca Adour Mk. 951 turbofan with FADEC
Primary Users: Royal Air Force, Indian Air Force , Royal Saudi Air Force , Royal Australian Air Force , South African Air Force
Status: In service
Wikipedia Article (URL): en.wikipedia.org/wiki/BAE_Systems_Hawk
Flat Wing Span (m): 9.7536
Wake Category: M
Aircraft Engine: Rolls-Royce Turbomeca Adour
Number of Engines: 1