Overview
The Kawasaki C-2 is a twin-engine military transport developed for the Japan Air Self-Defense Force. Introduced in the 2010s, it replaced older transport aircraft with improved range and payload. The aircraft supports strategic airlift missions.
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Specifications
Units
- Engine
- 2 × General Electric CF6-80C2K1F
- Engine type
- Turbofan
- Thrust
- 2 × 59,740 lbf · 266 kN
- Avionics
- —
- Wing tips
- No winglets
- Seats
- 3
- Crew
- —
- Cabin width
- 13 ft 1 in · 4.00 m
- Cabin height
- 13 ft 1 in · 4.00 m
- Cabin length
- 52 ft 6 in · 16.00 m
- Exterior length
- 144 ft 0 in · 43.90 m
- Tail height
- 46 ft 7 in · 14.20 m
- Fuselage diameter
- 16 ft 5 in · 5.00 m
- Wing span
- 145 ft 8 in · 44.40 m
- Baggage volume
- 8,864 ft³ · 251.0 m³
- Gross weight
- —
- Empty weight
- —
- Max takeoff weight
- 311,500 lb · 141,500 kg
- Max landing weight
- —
- Max payload
- 83,000 lb · 37,600 kg
- Fuel capacity
- 11,350 gal · 43,000 L · 34,400 kg (Jet A)
- Max cruise speed
- 500 kt · 575 mph · 926 km/h
- Maximum speed
- —
- Cruise speed
- —
- Approach speed
- —
- Range
- 5,400 nm · 6,210 mi · 10,000 km
- Fuel burn
- —
- Ceiling
- 40,000 ft · 12,200 m
- Rate of climb
- 3,500 ft/min · 18 m/s
- Takeoff distance
- 1,640 ft · 500 m
- Landing distance
- 1,640 ft · 500 m
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