Credit
Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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BSupport aircraft
Tanker (aircraft) / Transport, Overwatch / Ground support (Harvest HAWK variant)
At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
KC-130J · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Lockheed Martin KC-130 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Tanker (aircraft) / Transport, Overwatch / Ground support (Harvest HAWK variant)[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Air Tractor[source] | Lockheed Lockheed Martin[source] |
| Status | Active[source] |
97 ft 9 in (29.79 m)[source]
AT-802 · 1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (
Single source1 × Pratt & Whitney PT6A -67AG turboprop , 1,350 shp (1,010 kW)[source]
KC-130J · 4 × Allison T56 and Rolls-Royce AE 2100D3 turboprop engines, 4,637 shp ( ) each
Single source4 × Allison T56 and Rolls-Royce AE 2100D3 turboprop engines, 4,637 shp (3,458 kW) each[source]
AT-802 · 850 ft/min (
Single source850 ft/min (4.3 m/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Active[source]
| Manufactured | 1990–present[source] | — |
|---|
| First flight | 1990[source] | — |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 42,000 lb (19,051 kg)[source] |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | root: NACA 64A318 ; tip: NACA 64A412[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Primary users | — | United States Marine Corps Royal Canadian Air Force[source] |
|---|
| Number built | — | KC-130B: 6 KC-130F: 46 KC-130H: 33 KC-130R: 14 KC-130T: 28 KC-130J: 53[source] |
|---|
| Introduction date | — | KC-130F: 1962 KC-130R: 1976 KC-130T: 1983 KC-130J: April 2004[source] |
|---|
| Retired | — | KC-130F (2006) KC-130R (2007) KC-130T (2021)[source] |
|---|
| Developed from | — | Lockheed C-130 Hercules Lockheed Martin C-130J Super Hercules[source] |
|---|
| Developed into | — | Lockheed Martin HC-130J Lockheed Martin MC-130J[source] |
|---|
| Fuel capacity | — | 61,364 lb (27,834 kg) (with external tanks)[source] |
|---|
| Propellers | — | 6-bladed Dowty R391 constant-speed fully feathering reversible-pitch composite propellers[source] |
|---|
| Take-off run | — | 3,127 ft (953 m) at 155,000 lb (70,307 kg)[source] |
|---|
Maximum take-off; KC-130J · Max takeoff weight
Single source