Flat Wing Aspect Ratio
7.8
Entry Into service
1974-12-01
Maximum Take-Off Weight
38.7 t (paragliders: kg)
Total Fuel Capacity
15200
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Kawasaki C-1 |
38.7 |
15200 |
3353 |
Similar airplanes
All data (29 fields)
- Name
- Kawasaki C-1
- Manufacturer
- Kawasaki Heavy Industries
- Description
- The Kawasaki C-1 (川崎 C-1) is a twin-engined short-range military transport aircraft developed and manufactured by the Japanese conglomerate Kawasaki Heavy Industries.
- ICAO Code
- C1
- First Flight
- 1970-11-12
- Entry Into service
- 1974-12-01
- Service End
- 2025-03-15
- Designer
- Kawasaki Heavy Industries
- Type
- Military transport aircraft
- Length (m)
- 29
- Height (m)
- 9.99
- Cockpit Crew
- 2
- Max Speed (km/h)
- 806
- Cruise Speed (km/h)
- 657
- Max Ceiling (m)
- 11580
- Rate of Climb (m/s)
- 17.75
- Capacity Description
- 8000 kg normal payload
- National Origin
- Japan
- Number Built
- 31
- Powerplant Description
- 2 × Pratt & Whitney JT8D-M-9 (Mitsubishi-built) low-bypass turbofans
- Primary Users
- Japan Air Self-Defense Force
- Status
- Retired
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Kawasaki_C-1
- Flat Wing Span (m)
- 30.6
- Flat Wing Area (m²)
- 120.5
- Flat Wing Aspect Ratio
- 7.8
- Wake Category
- M
- Aircraft Engine
- Pratt & Whitney JT8D
- Number of Engines
- 2