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At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
Ka-31 · rotors folded
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Kamov Ka-31 |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Airborne early warning and control[source] |
| National origin | United States[source] | — |
| Manufacturer | Air Tractor[source] | Kamov[source] |
| Status | Active[source] | In service, In production[source] |
| Manufactured |
12.5 m (41 ft 0 in) rotors folded[source]
AT-802 · Wingspan
Single source59 ft 3 in (18.06 m)[source]
Ka-31 · 2 ×
Single source2 × 15.9 m (52 ft 2 in)[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]
Ka-31 · 2 × Isotov TV3-117VMA turboshaft engines each take-off / contingency rating
Single source2 × Isotov TV3-117VMA turboshaft engines, 1,864 kW (2,500 hp) each take-off / contingency rating[source]
AT-802 · Wing area
Single source401.0 sq ft (37.25 m 2 )[source]
AT-802 · Service ceiling
Single source13,000 ft (4,000 m)[source]
AT-802 · 850 ft/min (
Single source850 ft/min (4.3 m/s)[source]
Ka-31 · on-station loiter at 3,500 m (11,500 ft)
Single source2 hours 30 minutes on-station loiter at 3,500 m (11,500 ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
1990–present[source] |
1985–present[source] |
| First flight | 1990[source] | 1987[source] |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | — |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | — |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | — |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Primary users | — | Russian Navy Indian Naval Air Arm People's Liberation Army Navy[source] |
|---|
| Number built | — | 28[source] |
|---|
| Introduction date | — | 1995[source] |
|---|
| Developed from | — | Kamov Ka-27[source] |
|---|
| Main rotor area | — | 397.2 m 2 (4,275 sq ft)[source] |
|---|