AIDC F-CK-1 Ching-kuo

AIDC F-CK-1 Ching-kuo
Državi	Tajvan
Vlogo	Lovska letala
Prvi let	28. maj 1989
Zgrajena	131

The AIDC F-CK-1 Ching-Kuo (kitajsko: 經 boš號戰, pinyin: Jīngguó Hào Zhànjī), splošno znano kot Avtohtoni obrambni borec (IDF), je večrolsko bojno letalo, imenovano po Chiang Ching-kuo, pokojnem predsedniku Republike Kitajske. Letalo je prvič poletelo leta 1989. Januarja 1994 je bila dostavljena zračnim silam Republike Kitajske, leta 1997 pa je vstopila v službo. Vseh 130 proizvodnih letal je bilo izdelanih do leta 1999.

Vir: AIDC F-CK-1 Ching-kuo na Wikipediji

F-CK-1 Ching Kuo Walk Around
Fotograf	Zhang Jingwei
Lokalizacijo	Neznano
Fotografije	76

F-CK-1 Ching Kuo 1

F-CK-1 Ching Kuo 2

F-CK-1 Ching Kuo 3

F-CK-1 Ching Kuo 4

F-CK-1 Ching Kuo 5

F-CK-1 Ching Kuo 6

F-CK-1 Ching Kuo 7

F-CK-1 Ching Kuo 8

F-CK-1 Ching Kuo 9

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General Characteristics and Design

The AIDC F-CK-1 Ching Kuo (named after the late ROC President Chiang Ching-kuo) is a Taiwanese (Republic of China) indigenous multirole combat aircraft. The program was initiated in the 1980s when the U.S. government, under pressure from China, refused to sell Taiwan advanced fighters like the F-16 or F-20. As a result, the Aerospace Industrial Development Corporation (AIDC) developed the F-CK-1 with substantial technical assistance from U.S. aerospace companies. The design features a blend of characteristics from contemporary U.S. fighters (F-16/F/A-18), utilizing a slightly unstable airframe and a modern triple-redundant full authority fly-by-wire flight control system. It is the lightest twin-engine fourth-generation fighter fielded globally.

Property	Typical Value (F-CK-1A)
Vlogo	Multirole Fighter / Air Superiority
National Origin	Taiwan (Republic of China)
proizvajalec	Aerospace Industrial Development Corporation (AIDC)
First Flight	28 May 1989
Posadke	1 (F-CK-1A) or 2 (F-CK-1B/D Trainer)
Dolžina	14.21 m (46 ft 7 in)
Peruti	9.46 m (31 ft 0 in)
Empty Weight	6,486 kg (14,300 lb)
Max Takeoff Weight	12,247 kg (27,000 lb)

Powerplant and Performance

Engines: Two ITEC/Honeywell F125-GA-100 (TFE1042-70) non-afterburning turbofan engines.
Thrust (Each): 27 kN (6,000 lbf) dry / 42 kN (9,500 lbf) with afterburner.
Maximum Speed: Mach 1.8 (approx. 2,220 km/h or 1,379 mph).
Range: 1,100 km (680 mi; 590 nmi) (with minimum external fuel).
Service Ceiling: 16,800 m (55,100 ft).
Thrust-to-Weight Ratio: Approx. 0.95 (clean) / 0.70 (maximum load).

Armament and Avionics

Internal Gun: 1 x 20 mm M61A1 6-barreled Gatling cannon (located on the starboard side of the fuselage).
Hardpoints: 6 total (2 under-fuselage, 4 under-wing) with a max external payload of 4,000 kg (8,800 lb).
Indigenous Missiles: The F-CK-1 is integrated with a variety of domestically produced weapons:
- Air-to-Air: Sky Sword I (TC-1) (short-range IR-guided) and Sky Sword II (TC-2) (medium-range active radar-guided).
- Air-to-Surface: Wan Chien air-to-ground cruise missile and Hsiung Feng III anti-ship missile (testing/integration ongoing).
Other Munitions: AGM-65 Maverick, Mark 82/84 General Purpose Bombs, and Mk-20 Rockeye II cluster bombs.
Radar: 1 x GD-53 Golden Dragon multi-mode monopulse pulse-Doppler radar, a derivative of the General Electric AN/APG-67 (developed for the F-20). The radar has look-down/shoot-down capability.