Credit
OTOMATICC · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Atlantique 2 · Length
Single source31.62 m (103 ft 9 in)[source]
Falcon 900B · Length
Configuration
| Specification | Bréguet 1150 Atlantic | Dassault Falcon 900 |
|---|---|---|
| Type | Maritime patrol aircraft[source] | Business jet[source] |
| Manufacturer | Breguet Aviation[source] | Dassault Aviation[source] |
| Status | Active service[source] | Active service, in production[source] |
| Primary users | French Navy German Navy Italian Air Force Royal Netherlands Navy[source] |
20.21 m (66 ft 4 in)[source]
Atlantique 2 · Height
Single source10.89 m (35 ft 9 in)[source]
Empty; Atlantique 2 · Empty weight
Single sourceGross; Atlantique 2 · Gross weight
Single sourceMaximum take-off; Atlantique 2 · Max takeoff weight
Single source25,700 kg (56,659 lb)[source]
45,000 kg (99,208 lb)[source]
46,200 kg (101,854 lb)[source]
Empty; Falcon 900B · Empty weight
Single sourceMaximum take-off; Falcon 900B · Max takeoff weight
Single sourceFalcon 900B · with 8 passengers
Single source7,400 km (4,600 mi, 4,000 nmi) with 8 passengers[source]
Atlantique 2 · 2 × Rolls-Royce Tyne RTy.20 Mk 21 2-spool turboprop engines (6,100 shp) each (equivalent)
Single source2 × Rolls-Royce Tyne RTy.20 Mk 21 2-spool turboprop engines, 4,500 kW (6,100 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]
Atlantique 2 · Endurance
Single source18 hours[source]
Atlantique 2 · 2,900 ft/min
Single source14.7 m/s (2,900 ft/min)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] |
| Number built | 87 Atlantique 1 28 Atlantique 2[source] | >500[source] |
|---|
| Manufactured | 1961–1987[source] | 1984–present[source] |
|---|
| Introduction date | 1965[source] | — |
|---|
| First flight | 21 October 1961[source] | 21 September 1984 ( 1984-09-21 )[source] |
|---|
| Capacity | 12 passengers or relief crew[source] | 19 passengers[source] |
|---|
| Stall speed | 167 km/h (104 mph, 90 kn) flaps down[source] | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] |
|---|
| National origin | — | France[source] |
|---|
| Developed from | — | Dassault Falcon 50[source] |
|---|
| Developed into | — | Dassault Falcon 2000 Dassault Falcon 7X[source] |
|---|
| Fuel capacity | — | 8,690 kg (19,160 lb)[source] |
|---|
| Aspect ratio | — | 7.63:1[source] |
|---|