STATUS: Active, In-Service
MANUFACTURER(S): Kawasaki Heavy Industries (KHI) - Japan
LENGTH: 144.03 feet (43.9 meters)
WIDTH: 145.67 feet (44.4 meters)
HEIGHT: 46.59 feet (14.2 meters)
WEIGHT (EMPTY): 134,041 pounds (60,800 kilograms)
WEIGHT (MTOW): 311,734 pounds (141,400 kilograms)
ENGINE: 2 x General Electric CF6-80C2K1F turbofan engines developing 59,740 lb of thrust each.
SPEED (MAX): 631 miles-per-hour (1,015 kilometers-per-hour; 548 knots)
RANGE: 6,214 miles (10,000 kilometers; 5,400 nautical miles)
CEILING: 40,026 feet (12,200 meters; 7.58 miles)
Detailing the development and operational history of the Kawasaki C-2 Tactical Military Transport Aircraft.
Entry last updated on 1/17/2019.
Authored by Staff Writer. Content ©www.MilitaryFactory.com.
With the need to modernize into an independent fighting force (apart from reliance on the United States) and keep in step with developments emerging from China, the Japanese military is eyeing success with its in-development Kawasaki "C-2" series twin-engine transport. The aircraft was born from a Japan Air Self-Defense Force (JASDF) requirement calling for a new, high-wing transport to replace its stock of propeller-driven 1950s-era Lockheed C-130 "Hercules" models and 1970s'era Kawasaki "C-1" jet-powered transport line. Reviewing several possible foreign-originated replacements ultimately left authorities with the decision to go the indigenous route and the C-X program was begun headed by Kawasaki Heavy Industries.
Development begat the intended product with its modern swept-back high-wings, deep fuselage, and traditional "T-style" tail unit. The flight deck sits behind a blunt nose cone assembly while the tubular fuselage is of a stout, wide design. The multi-wheeled main undercarriage legs sit under bulges in the lower regions of the fuselage with the wing mainplanes seated at the top of the aircraft. Each wing contains an underslung engine nacelle as well as a network of flaps and other required surface controls. The empennage is characterized by the high-mounted horizontal planes emerging from the sole vertical tail fin. A powered cargo bay door is seated at the base of the tail section for access to the hold when loading/unloading goods. The typical crew arrangement is to feature three made up of two pilots and a loadmaster. The hold is cleared to carry infantry (including paratroopers), special missions equipment, up to eight cargo pallets, or a Sikorsky UH-60J (or similar) medium-lift helicopter. Empty weight is listed at 134,000lb with a Maximum Take-Off Weight (MTOW) nearing 265,000lb.
The high-wing approach grants the C-2 the strong lifting properties required for short-field operations, listed as one of the JASDF original requirements. The service plans to procure up to thirty of the aircraft to help add a tactically-flexible aircraft to its modernizing arsenal.
The aircraft was originally recognized under the "C-X" designation before being changed to the "XC-2". Production forms will take on the plain C-2 designation under the Kawasaki brand label. The C-2 has been developed alongside another Kawasaki product - the "P-X" for the Japanese navy - to help better manage program costs and development phases. This aircraft is intended as a maritime patrol platform for the Japan Maritime Self-Defense Force (JMSDF) and was introduced in 2013 while seeing at least thirteen airframes built to date (2014). The XC-2 itself has entered its flight testing phase, having recorded a first flight back on January 26th, 2010, though developmental/budgetary issues have pushed back its official service introduction - perhaps coming as soon as 2015 or slightly later.
With power derived from 2 x General Electric CF6-80C2K1F series turbofan engines outputting at 59,740lbf each, the C-2 will sport cruising speeds of around 550 miles per hour, a ferry range of 6,215 miles, and a service ceiling up to 40,000 feet. A commercial passenger-moving/cargo-hauling version is also being planned by Kawasaki for the civilian market.
June 2016 - The first C-2 aircraft was delivered marking the end of some 15 years of development. It was subsequently declared ready-for-service by the Japanese Ministry of Defense.
March 2017 - The Kawasaki C-2 formally began service with the Japan Air Self-Defense Force.
November 2017 - The C-2 was showcased at the Dubai Air Show to potential global customers looking to replace aging model lines such as the Lockheed C-130 Hercules.
December 2018 - The Kawasaki C-2 is a viable contender for a five-strong fleet requirement by the New Zealand Air Force. These would be used to succeed an aging fleet of C-130 cargo haulers.
January 2019 - The Japan Ministry of Defense has earmarked funds for five upcoming fiscal years to procure up to five Kawasaki Heavy Industries (KHI) C-2 transports.
January 2019 - Current operating squadrons of the C-2 include the Air Development and Test Wing and the 403rd Tactical Airlift Squadron of the 3rd Tactical Airlift Wing.
January 2019 - The Japan Ministry of Defense has revealed plans to develop a standoff "jamming" variant of its C-2 transport for service set to begin in or around 2025.
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Our Data Modules allow for quick visual reference when comparing a single entry against contemporary designs. Areas covered include general ratings, speed assessments, and relative ranges based on distances between major cities.
This entry's maximum listed speed (631mph).
Graph average of 562.5 miles-per-hour.
Graph showcases the Kawasaki XC-2's operational range (on internal fuel) when compared to distances between major cities.
Useful in showcasing the era cross-over of particular aircraft/aerospace designs.
Comm. Market HI*: 44,000 units
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