Credit
Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
An-2 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Antonov An-2 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Agricultural , utility aircraft and military transport aircraft[source] |
| National origin | United States[source] | Soviet Union[source] |
| Manufacturer | Air Tractor[source] | Antonov[source] |
| Status | Active[source] | In service |
12.4 m (40 ft 8 in)[source]
AT-802 · Wingspan
Single source59 ft 3 in (18.06 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]
An-2 · 1 × Shvetsov ASh-62IR 9-cylinder air-cooled supercharged radial piston engine
Single source1 × Shvetsov ASh-62IR 9-cylinder air-cooled supercharged radial piston engine, 750 kW (1,010 hp)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1990–present[source] | 1947–2001[source] |
|---|
| First flight | 1990[source] | 31 August 1947[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 12 passengers / 2,140 kg (4,718 lb)[source] |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | TsAGI R-11 (14%)[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | 50 km/h (31 mph, 27 kn) circa[source] |
|---|
| Designer | — | Oleg Antonov[source] |
|---|
| Primary users | — | Soviet Air Forces (historical) Russian Aerospace Forces Korean People's Army Air Force Ukrainian Air Force[source] |
|---|
| Number built | — | 18,000+[source] |
|---|
| Developed into | — | Antonov An-3 SibNIA TVS-2DTS[source] |
|---|
| Fuel capacity | — | 1,200 L (320 US gal; 260 imp gal)[source] |
|---|
| Upper wingspan | — | 18.2 m (59 ft 9 in)[source] |
|---|
| Lower wingspan | — | 14.2 m (46 ft 7 in)[source] |
|---|
| Propellers | — | 4-bladed constant-speed propeller[source] |
|---|
| Power/mass | — | 0.136 kW/kg (0.083 hp/lb)[source] |
|---|
| Fuel consumption | — | 185–200 L/h (49–53 gal/h; 41–44 imp gal/h)[source] |
|---|