Credit
Gartenfreuden (Wolfgang) · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
An-30 · Length
Single source24.26 m (79 ft 7 in)[source]
Falcon 20F · Length
Single sourceConfiguration
| Specification | Antonov An-30 | Dassault Falcon 20 |
|---|---|---|
| Type | Aerial cartography , reconnaissance and transport[source] | Business jet[source] |
| Manufacturer | Antonov[source] | Dassault Aviation[source] |
| Designer | Beriev[source] | — |
| Status | In limited service[source] | Out of production, in active service[source] |
| Primary users |
17.15 m (56 ft 3 in)[source]
Cruise; An-30 · Cruise speed
Single sourceMaximum; An-30 · Maximum speed
Single source540 km/h (340 mph, 290 kn)[source]
430 km/h (270 mph, 230 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-30 · 2 × Ivchenko AI-24T VT turboprop engines (2,803 shp) each equivalent
Single source2 × Ivchenko AI-24T VT turboprop engines, 2,090 kW (2,803 shp) each equivalent[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]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Russian Air Force Ukrainian Air Force People's Liberation Army Air Force Romanian Air Force[source] |
Federal Express (formerly) French Navy United States Coast Guard[source] |
| Number built | 123[source] | 512[source] |
|---|
| Manufactured | 1971 – 1980[source] | 1965–1991[source] |
|---|
| Introduction date | July 1968[source] | 3 June 1965[source] |
|---|
| First flight | 21 August 1967[source] | 4 May 1963[source] |
|---|
| Developed from | Antonov An-24[source] | — |
|---|
| Fuel capacity | 6,200 L (1,600 US gal; 1,400 imp gal)[source] | 5,200 L (1,100 imp gal; 1,400 US gal)[source] |
|---|
| Aspect ratio | 11.4:1[source] | 6.4:1[source] |
|---|
| Airfoil | root: TsAGI S-5-18; tip: TsAGI S-3-13[source] | — |
|---|
| Propellers | 4-bladed constant-speed propellers[source] | — |
|---|
| Take-off run | 710 m (2,329 ft)[source] | — |
|---|
| Landing run | 670 m (2,198 ft)[source] | — |
|---|
| Country of origin | Soviet Union[source] Soviet Union[source] | — |
|---|
| Developed into | — | Dassault Falcon 10 Dassault Falcon 50[source] |
|---|
| Capacity | — | 8–14 passengers[source] |
|---|
| Stall speed | — | 152 km/h (94 mph, 82 kn)[source] |
|---|
| National origin | — | France[source] |
|---|