艾德克 F - CK - 1 清国 | |
|---|---|
| 国家 | 台湾 |
| 作用 | 战斗机 |
| 首次飞行 | 1989年5月28日 |
| 建立 | 131 |
艾滋病中心 F-CK-1 清国 （中文：经国号战机；拼音：JīngguóHàoZhànjī），通常被称为“本土防御战斗机”（IDF），是一种以多位民国前总统蒋经国命名的多用途战斗机。该飞机于1989年进行了首次飞行。1994年1月交付给中华民国空军，并于1997年开始服役。到1999年，所有130架生产型飞机均已生产。
| F-CK-1 Ching Kuo Walk Around | |
|---|---|
| 摄影师 | Zhang Jingwei |
| 本地化 | 未知 |
| 照片 | 76 |
另请参阅：
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) |
|---|---|
| 作用 | Multirole Fighter / Air Superiority |
| National Origin | Taiwan (Republic of China) |
| 制造商 | Aerospace Industrial Development Corporation (AIDC) |
| First Flight | 28 May 1989 |
| 船员 | 1 (F-CK-1A) or 2 (F-CK-1B/D Trainer) |
| 长度 | 14.21 m (46 ft 7 in) |
| 翼展 | 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.
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