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Aeroprints.com · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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At a glance
Measured figures
Falcon 20F · Length
Single source17.15 m (56 ft 3 in)[source]
C-2 · Length
Single sourceConfiguration
| Specification | Dassault Falcon 20 | Kawasaki C-2 |
|---|---|---|
| Type | Business jet[source] | Military transport aircraft[source] |
| Manufacturer | Dassault Aviation[source] | Kawasaki Aerospace Company[source] |
| Status | Out of production, in active service[source] | In service, in production[source] |
| Primary users | Federal Express (formerly) French Navy United States Coast Guard[source] | — |
43.9 m (144 ft 0 in)[source]
Cruise; Falcon 20F · at 12,200 m (40,000 ft) (econ. cruise)
Single sourceMaximum; Falcon 20F · at 7,620 m (25,000 ft) (max cruise)
Single source862 km/h (536 mph, 465 kn) at 7,620 m (25,000 ft) (max cruise)[source]
750 km/h (470 mph, 400 kn) at 12,200 m (40,000 ft) (econ. cruise)[source]
Cruise; C-2 · / M0.8
Single sourceMaximum; C-2 · Maximum speed
Single sourceFalcon 20F · Range
Single source3,350 km (2,080 mi, 1,810 nmi)[source]
Falcon 20F · 2 × General Electric CF700 -2D-2 turbofans thrust each
Single source2 × General Electric CF700 -2D-2 turbofans , 20 kN (4,500 lbf) thrust each[source]
C-2 · 2 × General Electric CF6 -80C2K1F turbofan engines thrust each
Single source2 × General Electric CF6 -80C2K1F turbofan engines, 265.7 kN (59,740 lbf) thrust each[source]
Falcon 20F · Wing area
Single source41.00 m 2 (441.3 sq ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 512[source] | 21[source] |
|---|
| Manufactured | 1965–1991[source] | 2010–present[source] |
|---|
| Introduction date | 3 June 1965[source] | 30 June 2016[source] |
|---|
| First flight | 4 May 1963[source] | 26 January 2010[source] |
|---|
| Developed into | Dassault Falcon 10 Dassault Falcon 50[source] | — |
|---|
| Capacity | 8–14 passengers[source] | 32 t limited to + 2.5g ; 36 t limited to + 2.25g ; maximum payload 37.6 t Field Operation System or Truck Crane or 8 463L Pallets or 1 UH-60JA helicopter or 1 Type 16 maneuver combat vehicle wheeled tank destroyer[source] |
|---|
| Fuel capacity | 5,200 L (1,100 imp gal; 1,400 US gal)[source] | — |
|---|
| Aspect ratio | 6.4:1[source] | — |
|---|
| Stall speed | 152 km/h (94 mph, 82 kn)[source] | — |
|---|
| National origin | France[source] | Japan[source] |
|---|
| Primary user | — | Japan Air Self-Defense Force[source] |
|---|
| Minimum takeoff distance | — | 500 m (1,641 ft)[source] |
|---|