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C-1

C-1

Military Transport Aircrafts
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Basic Information
Name
C-1
Designation
C-1
Alternate Designation
Asuka (version powered by four turbofans), C-1Kai (ECM trainer), C-X (development program designation)
Equipment Type
Military Transport Aircrafts
Manufacturer
Kawasaki Heavy Industries (KHI), Mitsubishi Heavy Industries
Date of Introduction
1974
Description

The C-1 is turbofan-powered tactical military transport aircraft developed by a consortium led by Kawasaki in the late 1960s, early 1970s against a requirement from the Japan Air Self-Defense Force (JASDF) under C-X program. The other C-1 partners were Mitsubishi, Fuji and Nihon. The prototype first flew on November 12, 1970. JASDF took delivery of 31 C-1s between February 1974 and 1981. These freight aircraft are scheduled for replacement by a new turbofan-powered transport aircraft, also called the C-X, beginning in 2011. The Kawasaki C-1 freighter is powered by two JT8D-M-9 turbofans each rated at 14,500-lb of thrust. With a maxim takeoff weight of 45-t, its top speed is 805 kph and can transport an eight-ton payload over ranges of 1,200 kilometers. In the troops transport role, a single C-1 can transport 60 fully equipped infantrymen or 45 paratroops. The aircraft features a T tail and a large rear loading cargo ramp. The C-1 is also suitable for medical evacuation missions. JASDF also ordered two special variants: C-1Kai ECM trainer and Asuka powered by four above wing turbofans.

Air & Air Defense Specifications
Crew 4
Max Speed 805.0 km/h
Range 3355.0 km
Wingspan 30.60 m
Overview (Deagel)
Group Military Transport Aircrafts
Status Active
Also Known As Asuka (version powered by four turbofans), C-1Kai (ECM trainer), C-X (development program designation)
Origin Japan
Contractors Kawasaki Heavy Industries (KHI)*, Mitsubishi Heavy Industries
Initial Operational Capability (IOC) February 1974
First Flight November 12, 1970
Total Production 31
Specifications (Deagel)
Crew 4
Number of Engines 2
Paratroops 45
Stretchers 36
Troops 60
Area — Wing Area 121 square meter
Dimensions — Height 10.0 meter
Dimensions — Length 29 meter
Dimensions — Wingspan 30.6 meter
Mass — Cargo 7,900 kilogram
Mass — Empty Weight 24,300 kilogram
Mass — Max Takeoff Thrust 29,000 pound
Mass — Max Takeoff Weight 45,000 kilogram
Performance — Max Range 3,355 kilometer
Performance — Min Range 1,295 kilometer
Performance — Take Off Run Distance 640 meter
Speed — Climb Rate 3,495 fpm
Speed — Cruise Speed 704 kph
Speed — Economical Speed 658 kph
Speed — Top Speed at High Altitude 805 kph
Gear (Deagel)
Item 1 Turbofan Engines: JT8D (2)
Details
Country of Origin Japan
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
29 m
Width
30.6 m
Height
10 m
Weight
45000 kg
Operators (1)
Japan
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