Credit
Artem Katranzhi · CC BY-SA 2.0 · Resized · CC BY-SA 2.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Falcon 20F · Wingspan
Single source16.30 m (53 ft 6 in)[source]
Cruise; An-2 · Cruise speed
Single sourceMaximum; An-2 · Maximum speed
Single source258 km/h (160 mph, 139 kn)[source]
190 km/h (120 mph, 100 kn)[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 sourceAn-2 · 1 × Shvetsov ASh-62IR 9-cylinder air-cooled supercharged radial piston engine
Single source1 × Shvetsov ASh-62IR 9-cylinder air-cooled supercharged radial piston engine, 750 kW (1,010 hp)[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]
An-2 · 690 ft/min
Single source3.5 m/s (690 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Antonov An-2 | Dassault Falcon 20 |
|---|---|---|
| Type | Agricultural , utility aircraft and military transport aircraft[source] | Business jet[source] |
| Manufacturer | Antonov[source] | Dassault Aviation[source] |
| Designer | Oleg Antonov[source] | — |
| Status | In service[source] | Out of production, in active service[source] |
| Primary users | Soviet Air Forces (historical) Russian Aerospace Forces Korean People's Army Air Force Ukrainian Air Force[source] | Federal Express (formerly) French Navy United States Coast Guard[source] |
| Number built | 18,000+[source] | 512[source] |
| Manufactured | 1947–2001[source] | 1965–1991[source] |
| First flight | 31 August 1947[source] | 4 May 1963[source] |
| Developed into | Antonov An-3 SibNIA TVS-2DTS[source] | Dassault Falcon 10 Dassault Falcon 50[source] |
| Capacity | 12 passengers / 2,140 kg (4,718 lb)[source] | 8–14 passengers[source] |
| Fuel capacity | 1,200 L (320 US gal; 260 imp gal)[source] | 5,200 L (1,100 imp gal; 1,400 US gal)[source] |
| Upper wingspan | 18.2 m (59 ft 9 in)[source] | — |
| Lower wingspan | 14.2 m (46 ft 7 in)[source] | — |
| Airfoil | TsAGI R-11 (14%)[source] | — |
| Propellers | 4-bladed constant-speed propeller[source] | — |
| Stall speed | 50 km/h (31 mph, 27 kn) circa[source] | 152 km/h (94 mph, 82 kn)[source] |
| Power/mass | 0.136 kW/kg (0.083 hp/lb)[source] | — |
| Fuel consumption | 185–200 L/h (49–53 gal/h; 41–44 imp gal/h)[source] | — |
| National origin | Soviet Union[source] | France[source] |
| Introduction date | — | 3 June 1965[source] |
| Aspect ratio | — | 6.4:1[source] |