|
Entered service |
1981 |
|
Crew |
1 men |
|
Dimensions and weight |
|
Length |
21.59 m |
|
Wing span |
9.34
m |
|
Height |
5.41
m |
|
Weight (empty) |
10.3 t |
|
Weight (maximum take off) |
15.2 t |
|
Engines and performance |
|
Engines |
2 x Liyang (LMC) Wopen-13B II turbojets engines |
|
Traction (dry / with afterburning) |
2 x 47.1 / 68.7 kN |
|
Maximum speed |
2 337 km/h |
|
Service ceiling |
18 km |
|
Combat radius |
600 km |
|
Armament |
|
Cannon |
1 x 23-mm cannon with 200 rounds |
|
Missiles |
PL-2/3/5/7/9 or R-27R1 air-to-air missiles,
possibly C-801 anti-ship missiles |
|
Bombs |
250- 500- and 1 000-kg free-fall bombs |
|
Other |
57-mm rocket pods |
|
Built only
in small numbers up to 1987, the J-8 resembled little more than a
scaled-up twin-engined MiG-21 and had only a limited combat
capability. Revealed in 1984, the J-8 l Finback-A was an all-weather
development with a basic fire-control radar, 23-mm cannon and
missile armament.
The J-8 I first flew in prototype form in 1981 and
was followed by around 100 production aircraft (including J-8s
upgraded as J-8 Is). In 1981 work began on the much revised J-8 II
Finback-B with uprated engines, replacement of the nose inlet by two
lateral inlets, and the addition of a monopulse search radar. The
first of four J-8 II prototypes made its maiden flight in 1984 and
these have been followed by at least 24 production J-8 IIs.
SAC and
Grumman co-operated to develop an improved J-8 II with modernized
avionics, radar and weapons systems but this programme was
terminated by the USA in 1989. Despite this setback, SAC has
developed the upgraded F-8 IIM that represents a major advance.
Installation of a Phazotron Zhuk-8 II multi-mode pulse-Doppler radar
gives compatibility with R-27/AA-10 Alamo air-to-air missiles - the first
beyond visual range
weapons to be associated publicly with a Chinese combat aircraft.
Other possible air-to-air missiles may include an air-launched variant of the LY-60
SAM (itself a weapon that uses technology from the Italian Aspide)
and the Russian Vympel R-77/AA-12 Adder. The F-8 IIM also features a
hands on throttle and stick-equipped cockpit and uprated engines. Other proposed
indigenously-developed improvements include low-altitude navigation
and forward-looking infra-red/targeting pods, integral jamming system, a digital
fly-by-wire flight control system
and helmet-mounted sight. The first rebuilt F-8 IIM made its maiden
flight in 1996 and an unknown number have been built o date.
The F-8 IIM may have been developed for export, as an upgrade for the
PLAAF's J-8s, or simply as a testbed to integrate technologies
already in place on Chinese
Su-27s on an indigenous airframe. Around
100 J-8 I/IIs currently serve with four PLAAF regiments; the type
may also serve with the PLAN-AF.
|