The Kawasaki C-2 (previously XC-2 and C-X) is a mid-size, twin-turbofan engine, long range, high speed military transport aircraft developed and manufactured by Kawasaki Aerospace Company. In June 2016, the C-2 formally entered service with the Japan Air Self-Defense Force (JASDF).
The Kawasaki C-2 is a long range twin-engine transport aircraft. In comparison with the older C-1 that it replaces, the C-2 can carry payloads up to four times heavier, such as MIM-104 Patriot surface-to-air missile (SAM) batteries and Mitsubishi H-60 helicopters, and possesses six times the range.
The C-2 is being developed to meet the following requirements of the Ministry of Defense: a minimum payload of 26 tonnes, 120 metric ton (264,552 lb 132.275 short ton) take-off weight, ability to takeoff/land on short runways, (Requirement: 500m, almost same as C-1, e.g. Tachikawa—900 m, Kamigoto—800 m, Hateruma—800 m), a maximum payload of 37,600 kg whilst taking off from a 2,300 m Take-off Field Length at a 141 tonnes (310,851 lb 155.42 short ton) take-off weight, ability to fly international airroutes (Requirement: Mach 0.8+; JDA ruled out C-17 as a candidate by its lower cruising speed.
The Kawasaki C-2 is a long range twin-engine transport aircraft. In comparison with the older C-1 that it replaces, the C-2 can carry payloads up to four times heavier, such as MIM-104 Patriot surface-to-air missile (SAM) batteries and Mitsubishi H-60 helicopters, and possesses six times the range.The C-2 is being developed to meet the following requirements of the Ministry of Defense: a minimum payload of 26 tonnes, 120 metric ton (264,552 lb 132.275 short ton) take-off weight, ability to takeoff/land on short runways, (Requirement: 500m, almost same as C-1, e.g. Tachikawa—900 m, Kamigoto—800 m, Hateruma—800 m), a maximum payload of 37,600 kg whilst taking off from a 2,300 m Take-off Field Length at a 141 tonnes (310,851 lb 155.42 short ton) take-off weight, ability to fly international airroutes (Requirement: Mach 0.8+; JDA ruled out C-17 as a candidate by its lower cruising speed.
Conventional cargo aircraft cannot cruise at optimum altitude on commercial airroutes because of their lower cruising speed and are often assigned to lower altitude by ATC.), in-flight aerial refuelling and forward looking infrared systems.
The Kawasaki C-2 is powered by a pair of General Electric CF6-80C2K turbofan engines. While sharing fuselage components with the Kawasaki P-1, the fuselage of the C-2's is substantially larger to accommodate a vast internal cargo deck, which is furnished with an automated loading/unloading system to reduce workloads on personnel and ground equipment.
The forward fuselage and horizontal stabilizer is made of an internally-designed composite material, KMS6115. A tactical flight management system and head-up display is installed to reduce the challenges involved in flying at low altitudes or close to mountainous terrain. The C-2 is equipped with a full glass cockpit, fly-by-wire flight controls, a high-precision navigation system, and self protection systems. More details