Shenyang J-5

Chinese-built fighter aircraft introduced in 1957

Overview

Shenyang China ICAO: J5 1956–1969 Active

The Shenyang J-5 is a Chinese-built single-seat jet-powered interceptor and fighter aircraft based on the Soviet Mikoyan-Gurevich MiG-17. The Shenyang J-5 was exported as the F-5 and was initially named Dongfeng-101 and Type 56 before being named J-5 by 1964.

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Specifications

Units
Engine
1 × Wopen WP-5 (Chinese license name) / Klimov VK-1
Engine type
Jet
Thrust
7,600 lbf · 34 kN
Avionics
Shenyang Aircraft Corporation
Wing tips
No winglets
Seats
1
Crew
—
Cabin width
—
Cabin height
—
Cabin length
—
Exterior length
36 ft 5 in  ·  11.09 m
Tail height
12 ft 6 in  ·  3.80 m
Fuselage diameter
3 ft 11 in  ·  1.20 m
Wing span
31 ft 7 in  ·  9.63 m
Baggage volume
—
Gross weight
—
Empty weight
—
Max takeoff weight
13,700 lb  ·  6,200 kg
Max landing weight
—
Max payload
4,700 lb  ·  2,150 kg
Fuel capacity
670 gal · 2,500 L · 2,000 kg (Jet A)
Max cruise speed
610 kt  ·  702 mph  ·  1,130 km/h
Maximum speed
—
Cruise speed
—
Approach speed
—
Range
769 nm  ·  880 mi  ·  1,420 km
Fuel burn
—
Ceiling
54,100 ft  ·  16,500 m
Rate of climb
12,800 ft/min  ·  65 m/s
Takeoff distance
1,940 ft  ·  590 m
Landing distance
2,700 ft  ·  830 m
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China airforce Shenyang J5

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Operational Context

On July 19, 1956, the first Chinese-built Mig-17F, (serialized Zhong 0101) took its maiden flight piloted by Wu Keming. The aircraft produced several variants such as the Type 56, Dongfeng-101, Shenyang J-5, Shenyang J-5A, Chengdu JJ-5, and Shenyang J-5 torpedo bomber. Type 56 was the pre-service designation for the aircraft while the initial service name was Dongfeng-101.

The Shenyang J-5 was the first production aircraft redesignated in 1964. A total of 767 were built and all were single-seat versions. The J-5 is 3.8-meter tall and 11.09-meter long. It has a wingspan of 9.62 meters and a wing area of 22.6 square meters. The empty weight is 3,939 kg and the gross weight is 6,000 kg. It is powered by a single Wopen WP-5 turbojet engine which produces a maximum thrust of 5,700 lbf, and 7,600 lbf with afterburning. The aircraft has a maximum speed of 610 knots at 16,000 feet and a travel range of 769 nautical miles with drop tanks at 33,000 feet.

The Shenyang J-5A was the license production of the Radar-equipped MiG-17PF. A total of more than300 of this type were produced. This variant was still in service with the People’s Liberating Army Air Force.

The Chengdu JJ-5 was a twin-seat fighter trainer variant of the J-5. It was designed and developed by Chengdu Aircraft Corporation. The Chengdu JJ-5 was a combination of J-5 airframe, J-5A airbrakes, and the tandem twin-seat cockpit of the JJ-2 (MiG-15UTI). It has an external length of 11.5 meters. The empty weight is 4,080 kg and the gross weight is 6,125 kg. It was powered by a 5,010 lbf WP-5D non-afterburning turbojet. It has a maximum speed of 566 knots, a range of 660 nautical miles, a service ceiling of 46,900 feet, and a rate of climb of 5,300 feet per minute. Export variants were named FT-5.

The Shenyang J-5 torpedo bomber was a single aircraft carrying a single torpedo below the fuselage centerline. Central cannon was detached, as was some fuel storage capacity. Testing proved performance degradation was too great and further development was ditched.