About Project:FC-1 Xiaolong

ZhangKe

New Member
The Chengdu FC-1 Xiaolong (also known as Super-7) is the single-seat, single-engine, multi-role fighter aircraft developed by Chengdu Aircraft Industry Corporation (CAC) for export market. Currently three prototypes are flying. A joint venture between CAC and Pakistani Aeronautical Complex (PAC) will begin initial production of 16 aircraft in 2006. The designation of the aircraft in the Pakistani Air Force (PAF) is Joint Fighter-17 (JF-17) Thunder. It is still not clear whether the PLA Air Force will eventually acquire any of this aircraft.

PROGRAMME

In 1986 China signed a US$550 million agreement with Grumman to modernise its J-7 (MiG-21 Fishbed) fighter aircraft under the "Super-7" upgrade project. Western companies from the US and Britain were competing to provide the engine and avionics. The project was cancelled in early 1990, in the wake of the cooling of political relations with the West, as well as in response to a 40% increase in the cost of the project. However, Chengdu managed to continue the programme with its own resources and the project was re-branded as FC-1 (Fighter China-1).

Following the 1993 US sanction against China and Pakistan on the transfer of ballistic missile components and technology, problems of acquiring Western technology has driven Pakistan to seek helps from its Chinese ally. Beijing and Islamabad concluded a joint development and production agreement in June 1999 to co-develop the FC-1 fighter aircraft. According to the agreement, China Aviation Import and Export Corporation (CATIC) and Pakistan each contribute 50% of the development costs, which was estimated as about US$150 million. Chengdu was chosen to be the primary contractor, with Russian Mikoyan Aero-Science Production Group (MASPG) providing assistance in some design work as well as its RD-93 turbofan engine to power the aircraft.

The first FC-1 rolled out from the assembly line on 31 May 2003, and its 15-minute maiden flight took place on 24 August 2003. So far four prototypes have been built, with the second for static tests and the rest in flying tests. The initial production of 16 aircraft is expected to start in mid-2006, and the PAF has a requirement for 150 aircraft under the designation of the JF-17 to replace its Chengdu F-7P fighters in current service. Pakistani aviation industry will also be involved in the production of some avionics for the aircraft.

The FC-1/JF-17 targets mainly the international market as a potential replacement for the second-generation fighters such as the Northrop F-5 Tiger, Dassault Mirage III/5, Shenyang J-6, MiG-21/F-7 Fishbed, and Nanchang Q-5 aircraft. CATIC and CAC are trying to persuade the PLAAF to acquire additional FC-1s to reduce the unit price, but a firm contract has yet been reached. In addition, CATIC/CAC is also trying to promote the aircraft to other potential customers including Bangladesh, Egypt and Nigeria.

DESIGN

The FC-1/Super-7 was originally defined as a low-cost third-generation air-superiority fighter aircraft to replace the MiG-21/F-7 Fishbed and Northrop F-5 series in service with many developing countries. With the participation of MASPG, the aircraft was re-branded as a lightweight, high-performance, multirole attack fighter aircraft featuring fly-by-wire (FBW) flight-control, beyond-vision-range (BVR) combat capability and much improved aerodynamic performance. These has also steered the unit price of the aircraft up by 50%, from the original US$10 million to US$15 million.

The aircraft has delta wings and a conventional tail, and might be capable of aerial refuelling without significant modifications. The aircraft can be tailored to meet the different customers with various operational and budgetary requirements¡ªfrom low-cost options fitted with Chinese indigenously designed avionics to higher-performance options incorporated with Western developed weapons and avionics.

WEAPONS

The FC-1/JF-17 has 7 stores stations, including one under the fuselage, 4 under the wings, and 2 wingtip mounted, with up to 3,800kg weapon payload.

The aircraft is of beyond-vision-range (BVR) attack capability with the SD-10 medium-range air-to-air missile (MRAAM) developed by China Leihua Electronic Technology Research Institute (LETRI, also known as 607 Institute). The aircraft also carries two short-range AAMs on its wingtip-mounted launch rails. The options include U.S. AIM-9P and Chinese PL-6, PL-8, and PL-9.

The aircraft can carry a special pod allowing day/night delivery of laser-guided weapons. In addition, it can also carry unguided weapons such as iron bomb and unguided rocket launchers.

AVIONICS

The avionics suite onboard the FC-1/JF-17 is said to be Chinese design, comprising a head-up display (HUD), infra-red search-and-track system, night-vision goggle capability and ring-laser gyro inertial navigation system with GPS input. To achieve better aerodynamic performance, the FC-1/Super-7 is also equipped with a digital dual fly-by-wire (FBW).

The fire-control radar is expected to be selected among Israeli Elta-2032, Italian FIAR Grifo S-7, and Russian Phazotron Kopyo. The JF-17 Thunder fighters in service with the PAF will be fitted with the Italian Grifo S-7 fire-control radar, which has 25 working modes and a non-break-down time of 200 hours. The radar is capable of look-down, shoot-down, as well as for ground strike, but lacks multi-targets tracing and attacking capability.

POWERPLANT

One Russian-made RD-93 turbofans, rated 49.4kN dry or 81.4kN with afterburning. China has reportedly imported five RD-93s from Russia to power the prototypes, but agreement of further purchase and re-export of the engine in together with the fighter aircraft has yet been reached. China may seek to power the aircraft with an indigenously-developed powerplant.

SPECIFICATIONS

Crew: One
Wingspan: 9.00 m
Length: 14 m
Height: 5.10 m
Weight: Empty 6,321 kg; Normal take-off: 9,100 kg; Max take-off 12,700 kg; Max weapon payload 3,800 kg
Maximum Weapon Load: 3,600 kg
Maximum Speed: Mach 1.6
Range: Ferry range 3,000 km; Operational Radius 1,352 km
Service Ceiling: 16,500 m
Maximum Climb Rate: **
+G Limit: 8.5
 
Top