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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]
G-100 · Length
Single sourceConfiguration
| Specification | Dassault Falcon 20 | Gulfstream G100 |
|---|---|---|
| Type | Business jet[source] | Business jet[source] |
| Manufacturer | Dassault Aviation[source] | Gulfstream Aerospace[source] |
| Status | Out of production, in active service[source] | In service[source] |
| Primary users | Federal Express (formerly) French Navy United States Coast Guard[source] | — |
16.94 m (55 ft 7 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]
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]
G-100 · 2 × Honeywell TFE731 -40-R-200G turbofans thrust each
Single source2 × Honeywell TFE731 -40-R-200G turbofans , 18.9 kN (4,250 lbf) thrust each[source]
G-100 · 3,805 ft/min
Single source19.33 m/s (3,805 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built |
|---|
512[source] |
265: 145 Astra/G100 + 120 G150[source] |
| Manufactured | 1965–1991[source] | 1985–2017[source] |
|---|
| Introduction date | 3 June 1965[source] | — |
|---|
| First flight | 4 May 1963[source] | 1984[source] |
|---|
| Developed into | Dassault Falcon 10 Dassault Falcon 50[source] | Gulfstream G200[source] |
|---|
| Capacity | 8–14 passengers[source] | 6–9 passengers[source] |
|---|
| Fuel capacity | 5,200 L (1,100 imp gal; 1,400 US gal)[source] | 4,910 L (1,300 US gal; 1,080 imp gal) usable[source] |
|---|
| Aspect ratio | 6.4:1[source] | 8.8:1[source] |
|---|
| Stall speed | 152 km/h (94 mph, 82 kn)[source] | — |
|---|
| National origin | France[source] | — |
|---|
| Primary user | — | United States Navy[source] |
|---|
| Developed from | — | IAI Westwind[source] |
|---|
| Airfoil | — | IAI Sigma-2[source] |
|---|
| Fuel consumption | — | 1750 lb. per hour[source] |
|---|
| Country of origin | — | Israel[source]Gulfstream G100 · origin explicitly stated in the linked current national-inventory row; no inference from operator or shipyard |
|---|