Designer: Chengdu Aircraft Design Institute
Manufacturer: Chengdu Aircraft Industry Corporation
Operator: People's Liberation Army Air Force
Maiden Flight: 1998 (single-seat aircraft), 2003 (dual-seat aircraft)
Entry into Service: 2005
Number Built: 80
Unit Cost: RMB190m ($27.84m)
Wing Area: 33m²
Empty Weight: 9,750kg
Maximum External Load: 4,500kg
Loaded Weight: 14,250kg
Maximum Take-Off Weight: 19,277kg
J-10: 1 x Saturn Lyulka AL-31FN
Saturn AL-31FN M1 Thrust: 79kN, 123kN with afterburn
J-10 Super 10: 1 x Salyut AL-31FN M1
Salyut AL-31FN M1 Thrust: 132.5kN with afterburn
Internal Fuel Tanks Capacity: 4,950l
Maximum Speed – High Altitude: Mach 1.9 (2,327km/h)
Maximum Speed – Sea Level: Mach 1.2 (1,470km/h)
Combat Radius: 550km
Manoeuvrability, g Limits: -3g to +9g
Maximum Range: 1,850km
Air-to-Air Missiles: Luoyang
AL-31 Turbojet Engine: Saturn Lyulka
C-802 Land Attack and Anti-Ship: Cheta
The J-10 (Jian 10 or Fighter 10) is China's indigenously built multirole fighter aircraft developed by the Chengdu Aircraft Industry. Chengdu Aircraft Industry is part of the China Aviation Industry Corporation I (AVIC I). In the West the J-10 aircraft is known as the Vigorous Dragon.
It is estimated that up to 300 J-10 fighter aircraft will be manufactured. China's People's Liberation Army (PLA) includes the army, navy, air force and strategic rocket force. The air force (AFPLA) has 200 fighter and fighter ground attack squadrons and 120 strike fighter squadrons.
The J-10 aircraft is considered the replacement for the J-7 and Q-5. The air force currently operates about 250 J-7 (MiG-21) air defence and attack aircraft and about 500 Q-5 attack aircraft.
China formally announced the J-10 in February 2007. The existence of the J-10 was first reported in 1994, but the J-10 programme was started in 1988 and the first flight of the single seat aircraft took place in 1998. A two-seater variant made its first flight in 2003.
There are reports that the J-10 entered service in 2005 and is operational in single seater and two seater versions in at least two PLA air force squadrons.
The first native fourth-generation J-10 aircraft was unveiled by the air force in April 2010. Four J-10 fighter jets were showcased by the 24th fighter division of AFPLA. Pakistan will receive the first export versions of the J-10, up to 36 aircraft, by 2015. China and Pakistan have worked closely on the development of another fighter aircraft, the JF-17 or FC-1 light fighter aircraft.
The structure of the aircraft is based on a tail-less delta (triangular planform) wing, foreplanes and a sweptback vertical tail. There are two fixed, outwardly canted ventral (on the underside of the body) fins near the tail. The size and design of the J-10 are very similar to that of the Israeli Aircraft Industries Lavi fighter aircraft, which itself is similar to and derived technology from the USAF F-16 aircraft.
The horizontal close-coupled foreplanes (larger than those on the Lavi) on the forward fuselage improve the take-off and low-speed handling characteristics.
The J-10 has 11 external hardpoints: five hardpoints on the fuselage with one on the centreline and a pair of hardpoints on each side of the fuselage, and three hardpoints on each wing.
The outer wing stations carry air-to-air missiles such as the Chinese built Python 3 PL-8, P-11 or PL-12 or the Russian Vympel R-73 (AA-11 Archer) or R-77 (AA-12 Adder).
The PL-8 infrared homing short-range air-to-air missile is manufactured in China under a licensed production agreement by the China Academy (formerly the Luoyang Electro-optics Technology Development Centre) and is a variant of the Israeli Python 3 missile. The PL-11 is a licensed-manufactured variant of the MBDA Italy Aspide medium-range air-to-air missile.
The PL-12 missile is manufactured in China under a collaborative agreement with Russia. It uses the Russian AA-12 Adder missile technology configured with a Chinese-developed rocket motor to give a range of 50 miles and speed of Mach 4.
The aircraft can be armed with laser-guided bombs, the anti-ship YJ-8K or C-801K solid rocket powered missiles, the C-802 land attack and anti-ship turbojet-powered missiles manufactured by CHETA, and the YJ-9 anti-radiation missile.
A 23mm cannon is installed internally on the port side of the forward section of the fuselage above the nosewheel.
The aircraft could be fitted with a forward-looking infrared and laser target designator pod. The China Aviation Industry Corporation I (AVIC I) has displayed an exhibition model of the J-10 fitted with targeting pods, which would provide the capability of the J-10 to deploy laser and satellite navigation guided weapons.
Possible pulse Doppler radar fits include the Chinese Type 1473 radar, Russian Phazotron Zhuk-10PD or Zhemchug, the Chinese JL-10A, the Israeli IAI Elta EL/M-2023 or the Italian Galileo Avionica Grifo 2000.
The single-seat fighter aircraft is also being developed in a two-seat variant as a trainer aircraft and as an electronic warfare aircraft. The first flight of the two-seat variant was completed in 2003. The cockpit is fitted with a zero-zero ejection seat.
The aircraft has a digital fly-by-wire flight control system and HOTAS (hands-on throttle and stick) control on which the pilot has every control for combat incorporated into the two handholds.
Cockpit displays include a helmet-mounted weapon sight, a wide field of view head-up display and one full-colour and two monochrome liquid crystal multifunction displays. The avionics are served by a 1553B databus.
The aircraft is powered by the AL-31 turbojet engine supplied by Saturn Lyulka. The prototype aircraft and the first series of production aircraft are fitted with the AL-31FN developing 79kN and 123kN with afterburn, and which is the currently used in the Chinese Air Force Su-27 and Su-30 aircraft.
The more highly powered and advanced variant of the J-10, the Super-10, first reported in 2006, is fitted with the AL-31FN M1 supplied by Salyut. The AL-31FN M1 provides 132.5kN and is equipped with full authority digital engine control and a four-way swivelling exhaust nozzle for vectored thrust.
The aircraft carries a maximum of 4,950l of fuel internally, comprising 3,180l in the wing tanks and 1,770l in the fuselage tanks. A fixed refuelling probe for in-flight refuelling is installed halfway up the forward port side of the fuselage and just forward of the pilot.
Aerial refuelling of the J-10 is from a Xian H-6U tanker aircraft.
Additional fuel can be carried in auxiliary tanks on the centreline under the fuselage and on the innermost pair of the three sets of wing hardpoints.
The aircraft is equipped with tricycle-type landing gear. The nose unit has twin heels and retracts rearwards and the main units retract forward. The aircraft has a drogue parachute for landing.
The J-10 can fly at a maximum speed of 2,327km/h at high altitudes. Its maximum speed at sea level is 1,470km/h. The range and combat radius of the aircraft are 1,850km and 550km respectively. Its service ceiling is 18,000m. The aircraft weighs around 9,750kg and has a maximum take-off weight of 19,277kg.
Source: Airforce Technology
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