Unique in an industry dominated by turboprop aircraft, the Kawasaki C-1 is one of the few major short-range jet transports flying today. It began as part of a Japanese C-X specification for a transport to replace the US-built C-46 Commando which dated from World War II and was built by a consortium of companies including Mitsubishi, Fuji and Nihon. It was designed in the standard configuration of post-war transports, being a high-wing monoplane with a T-tail, a rear-loading ramp door, and a tricycle landing gear which is retractable into fuselage side fairings. Its twin jet engines are pylon-mounted beneath the wings making it seem like a miniature version of the much larger C-5 Galaxy. Although capable for its intended purpose, the relatively small maximum payload of the C-1 has limited its value (both domestically and for export) compared to other similar aircraft.
The prototype CX-1 had its maiden flight on 12 November 1970 and entered service in 1974 as the C-1. A mid life upgrade during the 1980s resulted in the C-1KA with a redesigned nose and upgraded avionics while an electronic surveillance variant is known as the EC-1. A number were also used for research purposes by Japan's National Aerospace Laboratory and the Japanese Defense Agency.
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NoneSucceeded by:
NoneDesign | C-1 |
Type | Transport |
Year | 1974 |
Crew | 5 |
Dimensions | |
Length | 29 m |
Height | 10 m |
Wing Span | 30.60 m |
Wing Area | n/a |
Weight | |
Empty | 23,320 kg |
Maximum | 45,000 kg |
Wing Loading | 373.4 kg/m² |
Performance | |
Speed | 806 km/h |
Ceiling | 11,580 m |
Range | 1,300 km |
Powerplant | |
Engine | 2 x JT8D-M-9 Mitsubishi 6,577 kgf |
Thrust/Weight | 0.51 |
Armament | |
Guns | - |
Payload | 11,900 kg |
Production | |
Built | 31 |
Total | 31 |