Ching kuo (idf) multirole fighter jet, taiwan
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The AIDC F-CK-1 Ching-kuo is a Taiwanese multirole fighter jet with air superiority capabilities. It has a shoulder-wing monoplane design and can withstand 9g forces. Powered by an AlliedSignal TFE1042 engine, the Ching-kuo is armed with a 20mm cannon and can carry missiles, bombs, and other weapons on six external hardpoints. With a top speed of Mach 1.8, the aircraft provides the Republic of China with defensive capabilities.
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The document describes a personal jet aircraft called the Recurve designed by students. The Recurve is intended to make private aircraft ownership more affordable and can carry a pilot and two passengers. It has a range of over 1,000 miles, can cruise at over 190 mph at 20,000 feet, and can takeoff and land on runways under 2,000 feet. The students selected a canard configuration for its suitability to amateur pilots while providing space for passengers.
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The document summarizes the Tomahawk cruise missile. It is a long-range, subsonic missile originally designed for medium-long range attacks from surface ships. Upgrades have improved its range and ability to retarget in flight. It carries conventional or nuclear warheads and uses TERCOM and DSMAC guidance with GPS and two-way satellite data links. The Tomahawk can be launched from US and UK naval ships and submarines and has a turbofan engine and rocket booster providing subsonic speed.
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Ching kuo (idf) multirole fighter jet, taiwan
- 1. { Ching-Kuo (IDF), Taiwan Multirole Fighter Jet
- 3. The AIDC F-CK-1 Ching-kuo (經國號戰機), commonly known as the Indigenous Defense Fighter (IDF), is a Taiwanese air superiority jet fighter with multirole capability named after Chiang Ching-kuo, the late President of the Republic of China. The airframe design was developed under the YingYan or Soaring Eagle programme. The aircraft is of shoulder-wing monoplane (single-wing) design, incorporating composite structure materials. The aircraft is built to withstand 9g loading. The Ching-Kuo fighter can be adapted to carry the TC-2A air-to-surface anti-radiation missile Introduction
- 5. The TFE1042 engine has been developed by the International Turbine Engine Corporation (ITEC), a joint venture between the Aerospace Industrial Development Corporation (AIDC) and AlliedSignal. The engine, weighing 1,360lb, delivers 41.1kN maximum thrust. The modular-designed engine has full digital electronic controls. The pressurised and air-conditioned cockpit has a Martin Baker Mark 12 zero zero ejection seat and a single-piece bubble canopy. The aircraft's radar is the Golden Dragon CD-53. The multi-mode pulse Doppler radar has look-down, shoot-down capability and can operate in air and sea search mode. Design
- 7. A 20mm M61A Vulcan cannon is installed on the starboard side of the fuselage with a Photo-Sonics gun camera. The aircraft has six hardpoints for carrying external stores, with two under the fuselage, one under each wing and one at each wingtip. For ground attack, the aircraft can be armed with rocket pods, bombs, cluster bombs or air-to-surface missiles such as Maverick. The fighter can also be adapted to carry the TC-2A air-to-surface anti-radiation missile, which uses both active and passive radar guidance. Weapons
- 9. General characteristics Length: 14.48 m (47 ft 6 in) Wingspan: 9 m (29 ft 6 in) Height: 4.42 m (14 ft 6 in) Wing area: 24.2 m2 (260 sq ft) Empty weight: 6,500 kg (14,330 lb) Gross weight: 9,072 kg (20,000 lb) Max takeoff weight: 20,000 kg (44,092 lb) Performance Maximum speed: Mach 1.8 (2,205 km/h) Range: 1,100 km (684 mi; 594 nmi) Service ceiling: 16,800 m (55,118 ft) Thrust/weight: 1.01 lbf/lb Specifications
- 10. http://en.wikipedia.org/wiki/AIDC_F-CK-1_Ching-kuo http://www.airforce-technology.com/projects/ching/ http://www.militaryfactory.com/aircraft/detail.asp?aircraf t_id=422 http://www.fighter-aircraft.com/aidc-f-ck-1-ching- kuo.html References
- 11. Thank You