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SUPER 7 / FC-1 / JF-17 THUNDER
 
OVER VIEW / HISTORY
 
The original project was started in 1986, when china signed an agreement with an American company Grumman to modernize china's aircraft J-7(F-7 / Mig-21), the agreement worth $550 million was then cancelled. China then contacted Pakistan in Feb 1992 for the joint venture and was accepted and started in Oct 1994. Pakistan shared half of its cost. Pakistan is expected to be the initial user of this plane and has planned to acquire 150 - 200 aircraft. Russia's Mikoyan Aero-Science Production Group (MASPG) is also providing technical expertise, it is also believed (in west) that super 7 is successor of the dropped Mig 33 aircraft. In the development of the plane several European countries are being considered as suppliers for the avionics. It uses Russian RD-93 turbofan, which is an upgrade of RD-33, this RD-93 turbofan is also used in Russian MiG-29. The aircraft will also be fitted with an in-flight refueling probe and a deck arrester hook. This increase its sticking range far beyond 3,000km. It is fitted with fire control radar Grifo S7, for the export version include state of the art GEC-Marconi Blue Hawk, Thomson-CSF RDY, Phanzotron Kapyo and Fiar Grifo S7. In addition to that it will include a 25° field of view HUD, two multi-functional displays and INS/GPS ( Global Positioning System). The aircraft  is designed to be fitted with vast array of weaponry. Weapon load includes short and medium range AAMs (Anti-Air Missiles) like  AIM-9P/PL-9/Magic 2 and PL-11/Aspide/AIM-7E etc, will also be equipped with SD-10 SD-10 active radar-homing AAM which has been under development at LETRI/607 Institute. SD-10 is expected to be in the same class as AMRAAM and the missile may have evolved from the earlier AMR-1/PL-12 design. Sd-10 AAM is specially designed for FC-1 aircraft In addition to that it includes new FBW system and a true BVR attack capability. The first prototype was completed in June 2003 and performed a taxi test in July 2003, It first flew on 3rd September 2003.

The plane was First known as FC-1, Super 7. and now it is also given the name JF-17 (Joint Fighter 17) "Thunder" for Pakistan Air Force (PAF).

 

SPECIFICATIONS

Crew One
Wing Span 9 m
Length 14 m
Height 5 m
Weight Empty 6,321 kg; Normal take-off: 9,100 kg
Max. TO. Weight 12,700 kg
Max. Weapon Load 3,600 kg
Max. Speed 1031 knots, Mach 1.8
Range Ferry range 3,000 km; Operational Radius 1,352 km, 864 nautical miles,
Service Ceiling 16,500 m
T-O Run 500 m
Landing Run 700 m
+G. Limit 8.5
Armament 23 mm GSh-23-2 twin-barrel cannon
6 - PL-7 AAM
6 - PL-10 AAMs
AGMs, bombs
 

Mock up of Super 7 standing at PAF base Kamra.
 


Views of Cockpit of JF-17, FC-1, Super 7.
 

A coloured view of JF 17 from all angles
 

JF-17 During its First Test Flight.
 
 
 
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