- Yes
- No
Background and History
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Origins:
The JF-17 Thunder project, also named “Fierce Dragon” in China, shares its origins in the ashes of the “Super 7” project, a destined debacle after the events of Tiananmen square that led to the western withdrawal from any cooperation.
In 1991 Chengdu Aircraft Co. (CAC) launched a new project designated FC-1 (Fighter China-1) that immediately saw new partners thanks to Russia and, eventually, Pakistan. This fighter project was in fact an export driven product, with Pakistan as the designated launch customer. The economical side of things was taken care of when in February 1998, the at the time Prime Minister of Pakistan, visited China and agreed that each country would contribute to 50% of the program’s funding, estimated around 150 million U.S. dollars. Both the PAF and PLAAF were interested in acquiring the fighter, with figures around 150 units for the former and 200 for the latter.
A Plethora of Delays:
Through its development and testing the project suffered due to a lack of funding and political tangles that at certain times completely blocked the normal cycle of work. Some of these “hiatuses” were so long and provided almost no information that some questions rose up about the survival of the project.
One of the issues was connected to the chosen powerplant of the JF-17, the Russian RD-93, a variant of the RD-33 specially produced for the new fighter. This critical component initially served as a saving grace for the project, but due to issues with exports from Russia it sometimes led to major pauses.
Another issue that plagued the fighter were its avionics. The acquisition of this equipment relied on the fragile relationship between Pakistan and the Western countries that at times became quite shaky and contributed to create uncertainties (One example would be Pakistan’s 1998 nuclear test).
There were also a bunch of structural and requirement changes provided to CAC by the PAF that led to the redesign of the fighter. A major shake-up (the one that probably killed the possibilities of seeing the PLAAF acquisition of this fighter) was India’s procurement of Su-30MKIs and the development of the Tejas, both factors that changed the PAF’s requirements to transform the JF-17 from a low-cost reliable platform to a much closer fighter to what the J-10 was (albeit at reduced payload, range and endurance).
Testing and Production:
The testing of the JF-17 was much more public compared to what we are used to when we think about China. In fact, the first FC-1 No. 01 was rolled out in 31 May 2003 and the event was featured in the Chinese and Pakistani media. There were 4 prototypes in total that underwent various kinds of testing, from low speed taxing to flight tests. The outcome of these tests was generally positive since the forth prototype, unseen until 2005, featured a number of modifications to the airframe aimed at diminishing the weight and fixing handling issues.
Production of the JF-17 started at CAC in 2006 and the first pre-production models were delivered to Pakistan in 2007. The official start of a fully Pakistani production line started in 2009 with the agreement for 42 additional airframes that were to be assembled by the Pakistani Aeronautical Complex (PAC) at Kamra.
Technical data
Specifications
Crew: 1
Length: 14.93 m
Wingspan: 9.45 m (with 2 wing-tip AAM)
Height: 4.72 m
Empty Weight: 6586 kg
Gross Weight: 9100 kg
Max Takeoff Weight: 12383 kg
Powerplant: 1 x RD-93 (RD-33 modification)
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Max Speed: Mach 1.6/1.9
Rate of Climb: 190 m/s
Ferry Range: 3482 km
Combat Radius: 1352 km
Service Ceiling: 16920 m
Maximum Payload: 3629 kg
G-Limit: +8.5 / -3
Armament
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1 x 23mm GSh-23-2 twin barrel cannon or 1 x 30mm GSh-30 cannon
7 Total Hardpoints [4 underwing, 2 on wingtips, 1 under fuselage]
PL-5E
SD-10 Medium-range (PL-12)
LT-2 PGB
LT-3 PGB
LS-6 500 kg PGB
GBU-12
MAR-1 anti-radiation missile
C-802K ASM (has been spotted)
WMD-7 IRST/laser designation pod
KG300G ECM pod
Avionics
KLJ-7 X-band pulse-Doppler radar (Later blocks used the KLJ-7A AESA radar)
MAWS (Similar to the J-10B and J-11B)
Type 634 quadruplex digital FBW system
HUD
Modern glass cockpit with 3 MFDs
MIL-STD-1553B databus and ring-laser gyro inertial navigational system.
CCIP
Flares and Chaff
Photos
Sources
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Book: Chinese Aircraft China’s Aviation Industry Since 1951
Book: Dragons Wings Chinese Fighter and Bomber Aircraft Development