IAI Lavi

Airplanes

Length

14.57 m

Flat Wing Span

8.78 m

Height

4.78 m

Flat Wing Area

33 m²

Max Speed

1912 km/h

Max Mach

1.8 Mach

Max Ceiling

15240 m

Number of Engines

Aircraft Engine

First Flight

1986-12-31

Number Built

Maximum Take-Off Weight

19.277 t (paragliders: kg)

Maximum Range

3700 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
IAI Lavi	19.277	3700

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
HAL Tejas Mk2	General Electric F414	14.65	8.5	Compare
General Dynamics X-62 VISTA	General Electric F110	14.8	9.8	Compare
General Dynamics F-16 Fighting Falcon	General Electric F110	14.9352	9.7536	Compare
Dassault Mirage 2000		14.36	9.13	Compare
Boeing–Saab T-7 Red Hawk	General Electric F404	14.0208	9.144	Compare
McDonnell Douglas AV-8B Harrier II	Rolls-Royce Pegasus	14.12	9.25	Compare

All data (22 fields)

Name: IAI Lavi
Manufacturer: Israeli Aircraft Industries
Description: The IAI Lavi (, "lion") is a single-engined fourth-generation multirole jet fighter developed in Israel, by Israel Aircraft Industries (IAI), during the 1980s.
First Flight: 1986-12-31
Designer: Israeli Aircraft Industries
Type: Multirole fighter
Length (m): 14.57
Height (m): 4.78
Cockpit Crew: 1
Max Speed (km/h): 1912
Max Ceiling (m): 15240
Rate of Climb (m/s): 254
Armament: 1 × 30 mm DEFA cannon
Max Mach (Mach): 1.8
Number Built: 3
Powerplant Description: 1 × Pratt & Whitney PW1120 afterburning turbofan
Status: Canceled in August 1987
Wikipedia Article (URL): en.wikipedia.org/wiki/IAI_Lavi
Flat Wing Span (m): 8.78
Flat Wing Area (m²): 33
Aircraft Engine: Pratt & Whitney PW1120
Number of Engines: 1