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Kfir (Lion Cub) Israeli Multi-Role Fighter

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Basic Information
Name
Kfir (Lion Cub) Israeli Multi-Role Fighter
Designation
Alternate Designation
Equipment Type
Manufacturer
Date of Introduction
1976
Description

The Israel Aircraft Industries Kfir (Hebrew: כְּפִיר, "Lion Cub") is an Israeli-built all-weather multirole combat aircraft based on the French Dassault Mirage 5, with Israeli avionics and an Israeli-built version of the General Electric J79 turbojet engine. The Kfir programme originated in the quest to develop a more capable version of the IAI Nesher, which was already in series production. After General De Gaulle embargoed the sale of arms to Israel, the IAF feared that it might lose qualitative superiority over its adversaries in the future, which were receiving increasingly advanced Soviet aircraft. The main and most advanced type of aircraft available to the IAF was the Mirage, but a severe problem developed due to the Mirage fleet's depletion due to attrition after the Six-Day War. Domestic production would avoid the problem of the embargo completely; efforts to reverse engineer and reproduce components of the Mirage were aided by Israeli espionage efforts to obtain technical assistance and blueprints from third party Mirage operators. Two power plants were initially selected for trials, the General Electric J79 turbojet and the Rolls-Royce Spey turbofan. In the end, the J79 was selected, not least because it was the same engine used on the McDonnell Douglas F-4 Phantom II, which the Israelis began to acquire from the United States in 1969, along with a license to produce the J79 themselves. The J79 was clearly superior to the original French Atar 09, providing a dry thrust of 49 kN (11,000 lbf) and an afterburning thrust of 83.4 kN (18,750 lbf). In order to accommodate the new powerplant on the Mirage III's airframe, and to deliver the added cooling required by the J79, the aircraft's rear fuselage was slightly shortened and widened, its air intakes were enlarged, and a large air inlet was installed at the base of the vertical stabilizer, so as to supply the extra cooling needed for the afterburner. The engine itself was encased in a titanium heat shield. A two-seat Mirage IIIBJ fitted with the GE J79 made its first flight in September 1970, and was soon followed by a re-engined Nesher, which flew in September 1971. An improved prototype of the aircraft, with the name Ra'am B ("Ra'am" means "Thunder"; the "Ra'am A" was the Nesher),[6] made its first flight in June 1973. It had an extensively revised cockpit, a strengthened landing gear, and a considerable amount of Israeli-built avionics. The internal fuel tanks were slightly rearranged, their total capacity being increased to 713 US gal (2,700 l). There were unconfirmed reports that a number of the original Mirage IIICs, re-engined with the J79 and given the name Barak ("Lightning"), took part in the Yom Kippur War of 1973, but some sources point out that there is no evidence that these aircraft ever existed.

Air & Air Defense Specifications
Crew 1
Variants
Kfir C1: Initial production model, leased to the US Navy and Marine Corps and re-designated F21A.
F-21A: Slightly modified C1, used to train us combat pilots in adversary tactics. Used by US Navy from 1985 to May 1988. Used by USMC from 1987 to Sep 1989.
Kfir C2: Revised airframe with foreplanes and nose strake added.
Kfir C7: Upgraded version with new avionics: wdns-391 weapons control system with stores management display, uprated GE J79-1JE engine and greater internal fuel capacity.
Kfir-2000: Designed as a cost-effective multi-role aircraft.
System
Alternative Designations See Variants
Crew 1
Engines General Electric J79-GE-1JE Turbojet. 17,750lbs thrust in the C2; 18,750lbs thrust in the C7.
Maximum take off weight 16,500 kg
Empty weight 7,285 kg
Ferry Range C2: 2,991km C7: 3,232km
Combat Radius': INA
Intercept Mission C2: 347km C7: 776
Combat Air Patrol C2: 699km C7: 882
Ground Attack C2: 768 C7: 1,186
Takeoff Run / Landing Roll (With Max Load) C2: 1,455m C7: 1,555m
Wingspan 8.2m
Height 4.6m
Standard External Payload C2: 4,277 C7: 5,775
Hardpoints C2: 7 C7: 9
Max Speed at Altitude 2,440; Mach 2.3
Max Speed at Sea Level 1,389; Mach 1
Takeoff / Landing Speed 220
Maximum G Forces 7.5 g's
Ceiling 17,680 m
Vertical Climb Rate 233 m/s
Fuel Internal: 3,243 liters; External: 4,700 liters
Cockpit pressurized, heated, and air conditioned Yes
Martin-Baker zero / zero ejection seat Yes
In-flight refueling Yes
IFF, ECM pods Yes
Radar warning reciever Yes
Chaff and Flares Yes
Weapons and Ammunition Types
Cannon 2x internal 30mm cannons
Other payload options Python / Shafrir / AIM-9: 2 each AGM-45 Shrike ARM: 2 each AGM-65 Maverick: 1 each Bombs: GBU-15 glide bomb: 1 each 227kg: 6 each 363kg or 454kg: 2 each 1,361kg: 1 each Fuel Tanks: Multiple options
Details
Country of Origin Israel
Category Multirole Aircraft
Air > Multirole Aircraft
Filter Label
K
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
Width
Height
4.6 m
Weight
16500 kg
Operators (2)
Colombia
Sri Lanka
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