FORCETALLY
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At a glance
Measured figures
Falcon 900B · Length
Single source20.21 m (66 ft 4 in)[source]
C-5M · Length
Single sourceConfiguration
| Specification | Dassault Falcon 900 | Lockheed C-5 Galaxy |
|---|---|---|
| Type | Business jet[source] | Strategic airlifter[source] |
| National origin | France[source] | United States[source] |
| Manufacturer | Dassault Aviation[source] | Lockheed Corporation Lockheed Martin[source] |
| Status | Active service, in production[source] | In service |
247 ft 1 in (75.31 m)[source]
C-5M · Height
Single source65 ft 1 in (19.84 m)[source]
Empty; Falcon 900B · Empty weight
Single sourceMaximum take-off; Falcon 900B · Max takeoff weight
Single source10,255 kg (22,608 lb)[source]
20,640 kg (45,503 lb)[source]
Empty; C-5M · Empty weight
Single sourceMaximum take-off; C-5M · Max takeoff weight
Single sourceFalcon 900B · Crew
Single sourceC-5M · typical (aircraft commander, first pilot, 2 flight engineers, 3 loadmasters) 4 minimum (pilot, copilot, two flight engineers) 8 when augmented (aircraft commander, 2 first pilots, 2 flight engineers, 3 loadmasters)
Single source7 typical (aircraft commander, first pilot, 2 flight engineers, 3 loadmasters) 4 minimum (pilot, copilot, two flight engineers) 8 when augmented (aircraft commander, 2 first pilots, 2 flight engineers, 3 loadmasters)[source]
Falcon 900B · with 8 passengers
Single source7,400 km (4,600 mi, 4,000 nmi) with 8 passengers[source]
C-5M · at maximum cargo capacity
Single sourceC-5M · with a 120,000 lb (54,431 kg) payload
Single sourceFerry; C-5M · with no cargo
Single source4,800 nmi (5,500 mi, 8,900 km) with a 120,000 lb (54,431 kg) payload, 2,300 nmi (4,260 km; 2,647 mi) at maximum cargo capacity[source]
7,000 nmi (8,100 mi, 13,000 km) with no cargo[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]
C-5M · 4 × General Electric F138-100 turbofan engines thrust each
Single source4 × General Electric F138-100 turbofan engines, 51,000 lbf (230 kN) thrust each[source]
C-5M · 2,100 ft/min (
Single source2,100 ft/min (11 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary users | French Air and Space Force Japan Coast Guard Nigerian Air Force Royal Malaysian Air Force[source] | — |
|---|
| Number built | >500[source] | 131 C-5A: 81 C-5B: 50[source] |
|---|
| Manufactured | 1984–present[source] | C-5A: 1968–1973 C-5B: 1985–1989[source] |
|---|
| First flight | 21 September 1984 ( 1984-09-21 )[source] | 30 June 1968 ( 1968-06-30 )[source] |
|---|
| Developed from | Dassault Falcon 50[source] | — |
|---|
| Developed into | Dassault Falcon 2000 Dassault Falcon 7X[source] | — |
|---|
| Capacity | 19 passengers[source] | 36 master pallets 463L or 281,000 lb (127,459 kg)[source] |
|---|
| Fuel capacity | 8,690 kg (19,160 lb)[source] | 341,446 lb (154,880 kg); 51,150 US gal (42,590 imp gal; 193,600 L)[source] |
|---|
| Aspect ratio | 7.63:1[source] | — |
|---|
| Stall speed | 158 km/h (98 mph, 85 kn) (wheels and flaps down)[source] | — |
|---|
| Primary user | — | United States Air Force[source] |
|---|
| Introduction date | — | June 1970 ( 1970-06 )[source] |
|---|
| Airfoil | — | root: NACA 0012.41 mod ; tip: NACA 0011 mod[source] |
|---|
| Thrust/weight | — | 0.26[source] |
|---|
| Take-off run | — | 5,400 ft (1,600 m)[source] |
|---|
| Landing run | — | 3,600 ft (1,100 m)[source] |
|---|