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 900B · Length
Single sourceConfiguration
| Specification | Antonov An-30 | Dassault Falcon 900 |
|---|---|---|
| Type | Aerial cartography , reconnaissance and transport[source] | Business jet[source] |
| Manufacturer | Antonov[source] | Dassault Aviation[source] |
| Designer | Beriev[source] | — |
| Status | In limited service[source] | Active service, in production[source] |
| Primary users |
20.21 m (66 ft 4 in)[source]
An-30 · Height
Single source8.32 m (27 ft 4 in)[source]
Empty; An-30 · Empty weight
Single sourceMaximum take-off; An-30 · Max takeoff weight
Single source15,590 kg (34,370 lb)[source]
23,000 kg (50,706 lb)[source]
Empty; Falcon 900B · Empty weight
Single sourceMaximum take-off; Falcon 900B · Max takeoff weight
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 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]
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] |
French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] |
| Number built | 123[source] | >500[source] |
|---|
| Manufactured | 1971 – 1980[source] | 1984–present[source] |
|---|
| Introduction date | July 1968[source] | — |
|---|
| First flight | 21 August 1967[source] | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Developed from | Antonov An-24[source] | Dassault Falcon 50[source] |
|---|
| Fuel capacity | 6,200 L (1,600 US gal; 1,400 imp gal)[source] | 8,690 kg (19,160 lb)[source] |
|---|
| Aspect ratio | 11.4:1[source] | 7.63:1[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] | — |
|---|
| National origin | — | France[source] |
|---|
| Developed into | — | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|
| Capacity | — | 19 passengers[source] |
|---|
| Stall speed | — | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] |
|---|