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-70 · Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Antonov An-70 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Military transport aircraft[source] |
| National origin | United States[source] | Soviet Union Ukraine[source] |
| Manufacturer | Air Tractor[source] | Kyiv Aircraft Production Plant[source] |
| Status | Active[source] | Completed state tests, open for production |
40.73 m (133 ft 8 in)[source]
Cruise; AT-802 · at 8,000 ft (2,440 m)
Single source221 mph (356 km/h, 192 kn) at 8,000 ft (2,440 m)[source]
AT-802 · Wing area
Single source401.0 sq ft (37.25 m 2 )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufactured | 1990–present[source] | 1991–1996 2012–2015[source] |
|---|
| First flight | 1990[source] | 16 December 1994[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | 300 troops or 206 stretcher cases / 47,000 kg (103,617 lb) max payload[source] |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | TsAGI P-202[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | 113 km/h (70 mph, 61 kn)[source] |
|---|
| Designer | — | Antonov Design Bureau[source] |
|---|
| Built by | — | Antonov Serial Production Plant[source] |
|---|
| Primary user | — | Ukrainian Air Force[source] |
|---|
| Number built | — | 2 prototypes[source] |
|---|
| Propellers | — | 14-bladed Aerosyla Stupino SV-27, 4.5 m (14 ft 9 in) diameter contra-rotating propeller (8-bladed forward; 6-bladed rear)[source] |
|---|
| Power/mass | — | 0.316 kW/kg (0.192 hp/lb) max[source] |
|---|
| Take-off field length | — | 1,800 m (5,900 ft)[source] |
|---|
| Landing field length | — | 2,000 m (6,600 ft)[source] |
|---|
| Take-off run STOL 30,000 kg (66,139 lb) payload | — | 600 m (2,000 ft)[source] |
|---|
| Take-off run STOL 35,000 kg (77,162 lb) payload | — | 915 m (3,000 ft)[source] |
|---|