Lightweight fighter

 

The LWF is intended to serve as a replacement for aircraft such as the F-5, A-4, Kifr, MiG-21, and MiG-23.  It is in roughly the same performance class as the F-20 Tigershark.

 

The aircraft bears a strong resemblance to the F-18 Hornet, and would in fact be powered by the same engine.  In order to keep development costs down, off-the-shelf components would be used as much as possible.  The avionics, cockpit, and radar would come from the F-16, for example.  Also, many operators of the aircraft the LWF is intended to replace (Israel, Turkey, and South Korea, for example) already operate F-16's, and parts commonality could have benefits in the training and maintenance category.

 

The aircraft has 7 weapons stations (1 centerline, 2 wingtip, and 4 underwing).  Possible loads are as follows:

Sta. 1 and 7 (wingtips)

1 AIM-9 Sidewinder

1 Python 3/4

1 AIM-132 ASRAAM

1 Derby (Israeli radar-guided AAM)

Sta. 2 and 6 (outboard underwing)

1 GBU-12/16/32

1 CBU-87/89/94/97

2 CBU-52/58

1 Mk-83

2 Mk-82

1 AGM-65 Maverick

1 AIM-9 Sidewinder

1 AIM-120 AMRAAM

1 Derby

1 Python 3/4

1 AIM-132 ASRAAM

3 Brimstone

Sta. 3 and 5 (inboard underwing)

1 AGM-88 HARM

2 GBU-12/32

1 GBU-10/16/24/31

1 CBU-87/89/94/97

3 CBU-52/58

1 Mk-84

2 Mk-83

3 Mk-82

1 AGM-65 Maverick

1 AIM-9 Sidewinder

1 AIM-120 AMRAAM

1 Derby

1 Python 3/4

1 AIM-132 ASRAAM

3 Brimstone

1 AGM-84 Harpoon/SLAM

1 AGM-154 JSOW

1 210 gal. external fuel tank

Sta. 4 (centerline)

1 GBU-10/12/16/24/31/32

1 CBU-87/89/94/97

2 CBU-52/58

1 Mk-84

2 Mk-82/83

1 AGM-154 JSOW

1 210 gal. external fuel tank

 

An additional hardpoint under the right engine inlet can mount targeting pods, such as the LANTIRN or HTS.

Loaded for antiarmor operations with 1 fuel tank, 12 Brimstones, and 2 AIM-9X.

 

A full air-to-air loadout of 4 AIM-120C and 2 Python 4.

Setup for strike, with 2 AIM-9X, 2 AIM-120C, 2 fuel tanks, 1 GBU-10, and a LANTIRN pod.

 

The leading-edge flaps, which can be seen in the Brimstone picture above, are operated automatically by the computer to suit the current flight condition, and can extend to a maximum of 20 degrees. 

The trailing-edge flaps are also computer-controlled, and can extend up to 15 degrees for maneuvering flight.  For takeoff and landing, they can extend further, to 30 and 45 degrees, respectively.

TEF's at full 45 degree extension.

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