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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]
C-130H · Length
Single sourceConfiguration
| Specification | Dassault Falcon 20 | Lockheed C-130 Hercules |
|---|---|---|
| Type | Business jet[source] | Tactical airlifter[source] |
| Manufacturer | Dassault Aviation[source] | Lockheed Corporation Lockheed Martin[source] |
| Status | Out of production, in active service[source] | In service[source] |
| Primary users | Federal Express (formerly) French Navy United States Coast Guard[source] | United States Air Force United States Navy United States Coast Guard United States Marine Corps |
97 ft 9 in (29.79 m)[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]
Cruise; C-130H · Cruise speed
Single sourceMaximum; C-130H · at 20,000 ft (6,100 m)
Single sourceC-130H · 4 × Allison T56 -A-15 turboprop engines, 4,590 shp ( ) each
Single source4 × Allison T56 -A-15 turboprop engines, 4,590 shp (3,420 kW) each[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]
C-130H · 1,830 ft/min (
Single source1,830 ft/min (9.3 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Number built | 512[source] | 2,700+ (as of June 2024)[source] |
|---|
| Manufactured | 1965–1991[source] | 1954–present[source] |
|---|
| Introduction date | 3 June 1965[source] | December 1956[source] |
|---|
| First flight | 4 May 1963[source] | August 23, 1954 ( 1954-08-23 )[source] |
|---|
| Developed into | Dassault Falcon 10 Dassault Falcon 50[source] | — |
|---|
| Capacity | 8–14 passengers[source] | 42,000 lb (19,000 kg) payload C-130E/H/J cargo hold: length, 40 ft (12.19 m); width, 9 ft 11 in (3.02 m); height, 9 ft (2.74 m). Rear ramp: length, 123 in (3.12 m); width, 119 in (3.02 m) C-130J-30 cargo hold: length, 55 ft (16.76 m); width, 9 ft 11 in (3.02 m); height, 9 ft (2.74 m). Rear ramp: length, 123 inches (3.12 m); width, 119 in (3.02 m) 92 passengers or 64 airborne troops or 74 litter patients with 5 medical crew or 6 pallets or 2–3 Humvees or 2 M113 armored personnel carriers 1 CAESAR self-propelled howitzer[source] |
|---|
| Fuel capacity | 5,200 L (1,100 imp gal; 1,400 US gal)[source] | — |
|---|
| Aspect ratio | 6.4:1[source] | — |
|---|
| Stall speed | 152 km/h (94 mph, 82 kn)[source] | — |
|---|
| National origin | France[source] | United States[source] |
|---|
| Variants | — | Lockheed AC-130 Lockheed DC-130 Lockheed EC-130 Lockheed EC-130H Compass Call Lockheed HC-130 Lockheed Martin KC-130 Lockheed LC-130 Lockheed MC-130 Lockheed RC-130 Lockheed WC-130 Lockheed L-100 Hercules Lockheed Martin C-130J Super Hercules[source] |
|---|
| Former operator · Afghanistan | — | Afghanistan[source] |
|---|
| Former operator · Angola | — | Angola[source] |
|---|
| Former operator · Belgium | — | Belgium[source] |
|---|
| Former operator · Brazil | — | Brazil[source] |
|---|
| Former operator · Honduras | — | Honduras[source] |
|---|
| Former operator · Rhodesia | — | Rhodesia[source] |
|---|
| Former operator · South Vietnam | — | South Vietnam[source] |
|---|
| Former operator · Spain | — | Spain[source] |
|---|
| Airfoil | — | root: NACA 64A318 ; tip: NACA 64A412[source] |
|---|
| Propellers | — | 4-bladed Hamilton Standard 54H60 constant-speed fully feathering reversible propellers, 13 ft 6 in (4.11 m) diameter[source] |
|---|
| Takeoff distance | — | 3,586 ft (1,093 m) at 155,000 lb (70,307 kg) max gross weight;[source] |
|---|
| Alternative designation | — | C-130 Hercules[source] |
|---|
| Reported operators | — |
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