|
Entered service |
2004 |
|
Crew |
1 men |
|
Dimensions and weight |
|
Length |
15.5 m |
|
Wing span |
9.7 m |
|
Height |
? |
|
Weight (empty) |
8.3 t |
|
Weight (maximum take off) |
18 t |
|
Engines and performance |
|
Engines |
1 x Lyulka-Saturn AL-31FN turbofan |
|
Traction (dry / with afterburning) |
1 x 79.43 / 122.58 kN |
|
Maximum speed |
Mach 2.2 |
|
Service ceiling |
? |
|
Ferry range |
? |
|
Combat radius |
? |
|
Armament |
|
Cannon |
23-mm cannon |
|
Missiles |
PL-12 and PL-8 air-to-air missiles |
|
Bombs |
500-kg laser-guided bombs, free-fall bombs |
|
Other |
90-mm unoperated rockets |
|
The J-10
multi-role fighter is the first Chinese-developed combat aircraft
that approaches Western fighters in terms of performance and
capabilities.
Development
of the J-10 began in 1988. It was intended to counter threat posed
by the Soviet forth-generation fighters - the
MiG-29 and
Su-27. The J-10 was initially planned as an air-superiority
fighter, however collapse of the Soviet Union and changing
requirements shifted the development towards a multi-role fighter.
Aircraft made it's maiden flight in 1998. The whole project was kept
under high secrecy. It is worth mentioning, that the first photos of
the J-10 came out only 3-4 years after the first flight. Some sources claim that it was influenced by the
IAI
Lavi. The J-10 multi-role fighter entered service with
Chinese air force in 2004, however it was first publicly revealed
only in 2006. Currently around 240 of these aircraft are in service. It is estimated that 300 fighter of this type will be
required for Chinese air force and possibly naval aviation too. A
number of countries, including Indonesia, Iran, Pakistan and
Thailand shown interest in purchasing this aircraft.
The J-10 has
a single engine. The first batch of about 50 aircraft is powered by
Russian AL-31FN turbofan engines. This batch was delivered to
Chinese air force between 2004 and 2006. An indigenous Taihang
turbofan is under development.
The J-10 has
beyond visual range air combat and surface attack capabilities.
Aircraft has 11 external hardpoints for a range of weapons.
Alternatively it can carry target acquisition, navigation pods or
auxiliary fuel tanks. It is worth mentioning that the J-10 has an
in-flight refueling capability.
The main
armament on the air-superiority missions are the PL-12 medium-range
active radar-homing air-to-air missiles. For close ranges it carries
the PL-8 infrared-homing missiles. For surface attack role the J-10
carries up to six 500-kg laser-guided bombs, free-fall bombs or
90-mm unoperated rocket pods. Aircraft is also completed with a
single-barrel 23-mm cannon.
The J-10 is
fitted with an indigenously designed pulse-doppler fire control
radar. It is capable of tracking 10 targets simultaneously and
attacking 4 of them. Estimated maximum detection range is 100 km.
Aircraft is fitted with a fly-by-wire system.
A two-seat
variant, the J-10S fighter-trainer, is available. It is identical to
the single-seat variant, but has a stretched fuselage to accommodate
second pilot seat. The J-10S can be used for pilot training or as a
standard fighter. This aircraft maid it's maiden flight in 2003.
Variants
J-10B
multi-role fighter, with improved airframe and avionics. It is
likely to become a standard production model.
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