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
An-2 · Length
Single source12.4 m (40 ft 8 in)[source]
Falcon 900B · Length
Single sourceConfiguration
| Specification | Antonov An-2 | Dassault Falcon 900 |
|---|---|---|
| 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] | Active service, in production[source] |
| Primary users |
20.21 m (66 ft 4 in)[source]
Falcon 900B · Wingspan
Single source19.33 m (63 ft 5 in)[source]
An-2 · Height
Single source4.1 m (13 ft 5 in)[source]
An-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 900B · 3 × Honeywell TFE731 -5BR-1C turbofans thrust each
Single source3 × Honeywell TFE731 -5BR-1C turbofans , 21.13 kN (4,750 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.
Soviet Air Forces (historical) Russian Aerospace Forces Korean People's Army Air Force Ukrainian Air Force[source] |
French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] |
| Number built | 18,000+[source] | >500[source] |
|---|
| Manufactured | 1947–2001[source] | 1984–present[source] |
|---|
| First flight | 31 August 1947[source] | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Developed into | Antonov An-3 SibNIA TVS-2DTS[source] | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|
| Capacity | 12 passengers / 2,140 kg (4,718 lb)[source] | 19 passengers[source] |
|---|
| Fuel capacity | 1,200 L (320 US gal; 260 imp gal)[source] | 8,690 kg (19,160 lb)[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] | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[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] |
|---|
| Developed from | — | Dassault Falcon 50[source] |
|---|
| Aspect ratio | — | 7.63:1[source] |
|---|