In the late 1970s, Israeli thinking began to focus on upgrading its stock of aging Douglas A-4 "Skyhawk" and IAI "Kfir" fighters / fighter-bombers through a more modern design centered on low-cost and low-complexity. The Israeli Air Force (IAF) requirement was for three hundred such aircraft with a collection of these to include two-seat trainer types. As Israel lived in a constant state of war with its Arab neighbors, time was of the essence.
Development began in early 1980 and the general design was initially influenced directly by IAF input. The new lightweight aircraft would carry inherent ground attack functionality while retaining full air-to-air combat capabilities and there grew the possibility to evolve the design into an advanced jet trainer. It was hoped that much of the aircraft could be developed and produced locally to help make Israel militarily more self-sufficient (and add to its economic power). Because of experience with Pratt & Whitney engines in other IAF aircraft, this brand would power the new jet.
Israel Aircraft Industries (IAI) had a history producing sound, viable military platforms for the IAF and the company headed development of what became known as the "Lavi" ("Young Lion" in Hebrew). Engineers elected for a "canard delta" planform in which the wing mainplanes were of considerable surface area so as to negate the need for horizontal tailplanes. Canards, small, variable-angle wings were affixed ahead of the mainplanes near the cockpit offering exceptional agility. The nose assembly was well-pointed and housed radar with the cockpit seated aft of this under a large, clear canopy offering excellent vision. The fuselage became well-contoured for extreme aerodynamic efficiency and large ventral strakes were fitted under the tail with a single vertical fin over it. Powered by a single turbofan engine, a single exhaust port was featured at rear with a ventral intake located under the cockpit floor. The undercarriage was of a conventional tricycle arrangement. An integral in-flight refueling probe was to become a standard fit for the aircraft. Composites were used in about 22% of the aircraft's construction.
The form of the Lavi was very much in tune with that of the American General Dynamics (now Lockheed) F-16 "Fighting Falcon" save for the use of a delta-wing configuration (it was also lighter and dimensionally smaller). Many other design qualities seemed to come from the F-16 which is of no surprise - the IAF adopted the lightweight multirole fighter and put it through its paces in the many Israeli-Arab conflicts in the decades that followed. The United States also served as a major partner to the Lavi's development. The F-16 - along with the McDonnell Douglas (now Boeing) F-15 "Eagle" still form the primary over-battlefield component of the IAF pending the arrival of more advanced types such as the Lockheed F-35 "Lightning II".
Three Lavi prototypes were eventually completed - the first two representing a two-seat form (the remaining three were to mark single-seat models). A first flight was had on December 31st, 1986 and the second prototype followed into the air in March of 1987. Power came from a single Pratt & Whitney PW1120 afterburning turbofan engine developing 20,600 pounds of thrust, providing for a maximum speed of 1,220 miles per hour, a range out to 2,300 miles, a service ceiling of 50,000 feet and a rate-of-climb reaching 50,000 feet-per-minute. Digital Fly-By-Wire (FBW) controlling made the inherently unstable delta canard configuration flyable and highly agile. The aircraft was powerful, fast and could present a formidable multi-role player in the inventory of the IAF.
Despite the steam being gained by the Lavi project, there were those within the Israeli ranks that did not champion the product as they saw the existing, readily-available F-16 could already accomplish all that was to be handled by the Lavi. Additionally, there were elements within the United States government and defense industry, particularly competing aviation concerns, that saw the Lavi as a direct threat to the global market share - particularly if Israel had decided to showcase its new aircraft on the world stage.
Under political pressure from the United States, a vote was held by the Israeli government which saw the Lavi narrowly cancelled. The United States rewarded the country by offering concessions through future military deals as well as continued regional support. This then led to the procurement of ninety F-16 (C-models) Fighting Falcons and effectively ended the Lavi program in 1987 - leaving just two prototypes and three incomplete airframes to show for the work. A third prototype joined the stock when parts from the forth and fifth airframe were cannibalized. This addition was used solely in the technology demonstration role to trial and evaluate key systems and subsystems used in other programs. The two remaining prototypes were saved from the scrapman's torch by becoming preserved showpieces.
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(OPERATORS list includes past, present, and future operators when applicable)
✓Air-to-Air Combat, Fighter
General ability to actively engage other aircraft of similar form and function, typically through guns, missiles, and/or aerial rockets.
✓Close-Air Support (CAS)
Developed to operate in close proximity to active ground elements by way of a broad array of air-to-ground ordnance and munitions options.
✓X-Plane (Developmental, Prototype, Technology Demonstrator)
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.
✓Training (General)
Developed ability to be used as a dedicated trainer for student pilots (typically under the supervision of an instructor).
Length
47.8 ft (14.56 m)
Width/Span
28.8 ft (8.78 m)
Height
15.7 ft (4.78 m)
Empty Wgt
15,498 lb (7,030 kg)
MTOW
42,505 lb (19,280 kg)
Wgt Diff
+27,007 lb (+12,250 kg)
(Showcased structural values pertain to the base IAI Lavi (Young Lion) production variant)
(Showcased performance specifications pertain to the base IAI Lavi (Young Lion) production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
STANDARD:
1 x 30mm DEFA internal cannon
OPTIONAL:
Up to 16,000lb of externally-held stores held across eleven total hardpoints - seven under-fuselage and four-underwing as well as wingtip mounts (wingtip mounts reserved for short-ranged AAMs only).
Supported Types
(Not all ordnance types may be represented in the showcase above)
Lavi - Base Series Name; three prototypes completed.
General Assessment
Firepower
Performance
Survivability
Versatility
Impact
Values are derrived from a variety of categories related to the design, overall function, and historical influence of this aircraft in aviation history.
Overall Rating
The overall rating takes into account over 60 individual factors related to this aircraft entry.
74
Rating is out of a possible 100 points.
Relative Maximum Speed
Hi: 1300mph
Lo: 650mph
This entry's maximum listed speed (1,221mph).
Graph average of 975 miles-per-hour.
City-to-City Ranges
NYC
LON
LON
PAR
PAR
BER
BER
MOS
MOS
TOK
TOK
SYD
SYD
LAX
LAX
NYC
IAI Lavi (Young Lion) operational range when compared to distances between major cities (in KM).
Max Altitude Visualization
Design Balance
The three qualities reflected above are altitude, speed, and range.
Aviation Era Span
Showcasing era cross-over of this aircraft design.
Unit Production (3)
3
36183
44000
Compared against Ilyushin IL-2 (military) and Cessna 172 (civilian).
Ribbon graphics not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective aerial campaigns / operations / aviation periods.
Images Gallery
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Israel (cancelled)
