Chinese fourth-generation carrier-based multirole fighter
The
Shenyang J-15
(
Chinese
: ?-15), also known as
Flying Shark
(
Chinese
:
??
;
pinyin
:
F?ish?
; NATO reporting name:
Flanker-X2
,
[3]
) is a Chinese
all-weather
,
twinjet
,
carrier-based
fourth-generation
[4]
multirole
fighter aircraft
developed by the
Shenyang Aircraft Corporation
(SAC) and the
601 Institute
, specifically for the
People's Liberation Army Naval Air Force
(PLANAF) to serve on
People's Liberation Army Navy
's
aircraft carriers
.
The T-10K-3, an unfinished prototype of the
Su-33
,
[5]
was acquired by SAC from
Ukraine
[6]
in 2001 and is claimed to have been studied extensively and
reverse-engineered
, with development on the J-15 beginning immediately afterward.
[7]
[8]
While the J-15 appears to be structurally based on the prototype of Su-33, the fighter features indigenous Chinese technologies as well as
avionics
from the
Shenyang J-11B
program.
[9]
In February 2018, discussions about replacing the aircraft appeared in several Chinese media outlets including
Xinhua
and China's main military newspaper, discussing that it belongs to the 4th- or
4.5-generation fighters
. Thus, the J-15 is viewed as an interim carrier-based fighter until a
fifth-generation
successor enters service, one that may be based on the
Chengdu J-20
or
Shenyang FC-31
.
Development
[
edit
]
China has sought to purchase
Su-33s
from Russia on several occasions ? an unsuccessful offer was made as late as March 2009
[10]
? but negotiations collapsed in 2006 after it was discovered that China had developed a modified version
[11]
[12]
[13]
of the
Sukhoi Su-27
SK, designated the
Shenyang J-11B
,
[14]
[15]
in violation of
intellectual property
agreements. However, according to Chinese sources, the reason China withdrew from talks was that Russia wanted large payments to re-open Su-33 production lines and insisted on a Chinese purchase of at least 50 Su-33s, about which China was reluctant as it believed the aircraft would become outdated in a few years. China hence decided on an indigenous variant instead of continuing to assemble the J-11, the licensed Chinese version of
Su-27
.
[16]
[17]
The J-15 program was officially started in 2006 with the codename Flying Shark.
[18]
The program goal was to develop a naval-capable fighter aircraft from the Shenyang J-11, with technologies reverse-engineered from T-10K-3, a Soviet Su-33 prototype acquired from
Ukraine
.
[19]
The first J-15 prototype made its
maiden flight
on August 31, 2009, believed to be powered by Russian-supplied
Saturn AL-31
turbofan engines
.
[9]
Video and still images of the flight were released in July 2010, showing the same basic airframe design as the Su-33.
[20]
On May 7, 2010, the aircraft conducted its first
takeoff
from a simulated
ski-jump
on land.
[9]
On November 25, 2012, the aircraft successfully performed its first
takeoff and landing
on
Liaoning
,
[21]
China's first operational
aircraft carrier
.
The
twin-seat
variant, J-15S, made its maiden flight on November 4, 2012. The twin-seat
electronic warfare
variant, similar to the role of
United States Navy
's
EA-18G Growler
, dubbed J-15D, took its maiden flight in 2018.
[22]
In 2016, the J-15T prototype with
CATOBAR
capability began test flight at
PLA Navy
land-based catapult facilities.
[23]
In November 2020,
Jane's
reported that SAC had produced a second prototype of the J-15T fighter aircraft.
[24]
In 2021, military analysts reported that China has worked on an upgraded variant called J-15B,
[25]
[26]
with new avionics, engines, and
CATOBAR
launch capability. The upgrade variant of J-15 is capable of launching newer
PL-10
and
PL-15
missiles.
[27]
In November 2022, a production J-15 powered by the
Shenyang WS-10
, possibly the WS-10B, appeared in Chinese media.
[28]
It was the last indigenous Chinese combat aircraft to replace the AL-31;
[29]
possibly due to
navalisation
.
[30]
According to Chinese observers, compared to the AL-31 the WS-10 had superior safety, reliability, and service life, aspects which are magnified by the constraints of carrier aviation.
[31]
Design
[
edit
]
The airframe of the J-15 is structurally reinforced for carrier landing and launching, with the addition of a tailhook and strengthened landing gears.
[18]
The aircraft incorporated a higher portion of composite materials than the
Sukhoi Su-33
to save weight and improve aerodynamic performance, allowing for a slower landing speed compared to Su-33.
[19]
An article in the
China SignPost
believes the J-15 "likely exceeds or matches the
aerodynamic
capabilities of virtually any fighter aircraft currently operated by regional militaries, except for the
U.S.
F-22 Raptor
", alleging that the J-15 likely possesses a 10% greater
thrust-to-weight ratio
and 25% lower
wing loading
than the
F/A-18E/F Super Hornet
.
[32]
[33]
However, one of the authors of that same article described the J-15 in another article as no game changer; the reliance on ski-jump launches and lack of Chinese carrier-based
aerial refueling
capabilities are believed to greatly reduce its effective
combat range
.
[34]
In 2014, it was revealed that the J-15 is capable of aerial refueling, using the UPAZ-1 buddy refueling pod, which can be carried by another J-15.
[35]
Hu Siyuan of the
PLA National Defense University
said that "the current weak point of the J-15 is its Russian-made AL-31 engines, which are less powerful than that of the American
F-35
fighter".
[36]
The J-15's chief designer, Sun Cong of the National Committee of the Chinese People's Political Consultative Conference, has said that the J-15 could match the F/A-18 in bomb load, combat radius and mobility. However, in a similar statement, he said more work was required on its electronics and combat systems.
[37]
Rear Admiral
Yin Zhuo
stated that the aircraft's air combat capabilities were better than that of the F/A-18E/F Super Hornet. However, he also stated that its ability to attack land and sea targets was slightly inferior to the F/A-18E/F; it is also stated that its electronic equipment meets the standards of those on a
fifth-generation fighter
.
[38]
J-15 is capable of operating on the aircraft carrier
Liaoning
and her sister ship
Shandong
. The carriers have two launch positions. The waist position has a runway length of 195 m, and the two forward positions have a runway length of 105 m. The take-off weight of the J-15 depends on the launch position and carrier speed. For ship speed at 28 knots, J-15's maximum take-off weight is 33 tons (with 9 tons of internal fuel and a 6.5-ton external payload) for the waist position. The maximum weight is 28 tons (9-ton internal fuel and 1.5-ton external payload) for the forward position. However, when the carrier moves at 20 knots, MTOW at the waist position is reduced to 31 tons.
[1]
With the introduction of aircraft carrier
Fujian
and J-15B, MTOW will maintain at 33 ton at any launch position and ship speed.
Operational history
[
edit
]
On November 25, 2012, Chinese media announced that two J-15s had made successful
arrested landings
on the
Liaoning
aircraft carrier.
[39]
[40]
[41]
The first pilot to land on
Liaoning
was named as Dai Mingmeng (戴明盟).
[42]
Luo Yang
, the aircraft's head of production and designer, died the same day.
[43]
PLA Daily
newspaper indicated that the first five naval pilots (including Dai) conducted J-15 fighter landings and takeoffs. Test and training program officials confirmed the carrier-borne aircraft and special equipment for the landing flight had gone through strict tests, and fighter jets can be deployed on the carrier.
[44]
In December 2013, Chinese media reported that
mass production
of J-15s in full operational condition with combat markings had begun.
[45]
In January 2017, the carrier
Liaoning
, having returned to the
South China Sea
after its first deployment into the
Western Pacific
, conducted a series of take-off and landing drills with its squadron of embarked J-15 fighters.
[46]
In July 2018,
Lieutenant General
Zhang Honghe of the
PLAAF
stated that China was developing a new carrier-based aircraft to replace the J-15 due to its two crashes and a series of “unpardonable mechanical failures”. One problem with the aircraft is that it is the heaviest carrier-borne fighter in current operation anywhere, with an
empty weight
of 17,500 kg (38,600 lb) compared to the F/A-18E/F Super Hornet's 14,600 kg (though it is less than the
F-14 Tomcat
's weight of 19,800 kg). Weight problems are compounded when operating off
Liaoning
, as its
STOBAR
launch and recovery method further limits payload capacity.
[47]
[48]
Accidents
[
edit
]
- In April 2016, a J-15 crashed into the ocean after experiencing a flight control system failure. The pilot, Cao Xianjian,
ejected
shortly before impact, below the altitude needed for the parachute to function; he was severely injured upon landing.
[49]
- On 27 April 2016, a J-15 crashed during a simulated landing when a flight control system malfunction caused the aircraft to pitch up to 80 degrees. The pilot, Zhang Chao, ejected below the altitude needed for the parachute to function; he died from injuries sustained upon landing.
[50]
- In July 2017,
[51]
a J-15 suffered a left engine fire after
ingesting a bird
shortly after takeoff. The pilot, Yuan Wei, with the aid of instructions from air traffic controllers, performed an emergency landing and ground crews extinguished the fire.
[52]
Variants
[
edit
]
- J-15
(
NATO reporting name
Flanker-X2
):
[53]
[3]
Single-seat variant.
[22]
- J-15S
: Two-seat variant, first flown in 2012.
[53]
[22]
- J-15T
(
Flanker-X2
):
CATOBAR
operation prototypes, first seen in September 2016. Two were built.
[23]
[24]
- J-15D
(
Flanker-X2
): Two-seat
electronic warfare
variant with
EW
pods and other electronic equipment installed and
IRST
sensor removed.
[22]
Begun operational testing in December 2018.
[23]
[54]
- J-15B
: Improved J-15 incorporating
CATOBAR
launch capability from J-15T, fitted with modern
fifth-generation
avionics,
AESA
radar, new airframes, stealth coatings, and compatibility to launch
PL-10
and
PL-15
missiles. In flight testing.
[25]
[26]
Operators
[
edit
]
-
People's Republic of China
Specifications (estimated)
[
edit
]
Data from
Military Factory : Shenyang J-15 (Flying Shark) - Development and Operational History, Performance Specifications and Picture Gallery
[56]
[57]
General characteristics
- Crew:
1 or 2
- Length:
22.28 m (73 ft 1 in)
- Wingspan:
15.0 m (49 ft 3 in)
- Width:
7.4 m (24 ft 3 in) wings folded
- Height:
5.92 m (19 ft 5 in)
- Wing area:
67.84 m
2
(730.2 sq ft)
- Empty weight:
17,500 kg (38,581 lb)
- Gross weight:
27,000 kg (59,525 lb)
- Max takeoff weight:
32,500 kg (71,650 lb)
- Fuel capacity:
9,500 kg internal
- Powerplant:
2 ×
Saturn AL-31
[58]
afterburning turbofans, 122.6 kN (27,600 lbf) with afterburner
- Powerplant:
2 ×
WS-10B
[28]
afterburning turbofans, 89.17
[59]
kN (20,050 lbf) thrust each dry, 135
[28]
[60]
[61]
kN (30,000 lbf) with afterburner
Performance
- Maximum speed:
Mach 2.4
- Ferry range:
3,500 km (2,200 mi, 1,900 nmi)
- Service ceiling:
20,000 m (66,000 ft)
- Thrust/weight
:
0.93 with AL-31 (1.01-1.07 with WS-10B)
Armament
- 1 × 30 mm
GSh-30-1
cannon with 150 rounds
- Munitions on twelve external hardpoints with a capacity of 6,500 kg,
[62]
including:
Avionics
- Type 1493 radar
[63]
- J-15D and J-15B claimed to have
AESA
radar
[64]
- MIL-STD-1553B
bi-directional data bus
- Glass cockpit
- LCD screen
- 4-redundant 3-axis fly by wire
See also
[
edit
]
Related development
Aircraft of comparable role, configuration, and era
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[
edit
]
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.
External links
[
edit
]
|
---|
Ji?n "J"
(Fighter)
| |
---|
Export
| |
---|
Related
designations
|
|
---|
1
Unknown/not assigned
See also:
J-XX
|