Credit
Daniel VA · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
AT-802 · Length
Single source35 ft 11 in (10.95 m)[source]
Length
Single sourceConfiguration
| Specification | Air Tractor AT-802 | Boeing WC-135 Constant Phoenix |
|---|---|---|
| Type | Agricultural / Fire-fighting aircraft[source] | Atmosphere testing related to nuclear incidents[source] |
| National origin | United States[source] | — |
| Manufacturer | Air Tractor[source] | Boeing Military Airplanes Division[source] |
| Status | Active[source] | 3 aircraft in service (WC-135R)[source] |
139 ft 11 in (42.65 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]
4 × Pratt & Whitney TF33-P-9 (WC-135C) / Pratt & Whitney TF33-P-5 (WC-135W) turbofan engines thrust each
Single source4 × Pratt & Whitney TF33-P-9 (WC-135C) / Pratt & Whitney TF33-P-5 (WC-135W) turbofan engines, 16,050 lbf (71.4 kN) thrust 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.
| Manufactured | 1990–present[source] | — |
|---|
| First flight | 1990[source] | — |
|---|
| Variant | L3Harris OA-1K Skyraider II[source] | Boeing OC-135B Open Skies[source] |
|---|
| Capacity | 820 US gal (683 imp gal; 3,104 L)[source] | — |
|---|
| Aspect ratio | 8.8:1[source] | — |
|---|
| Airfoil | NACA 4415[source] | root: BAC 310/311/312; tip: BAC 313[source] |
|---|
| Stall speed | 91 mph (146 km/h, 79 kn) (power off, flaps down)[source] | — |
|---|
| Primary user | — | United States Air Force[source] |
|---|
| Number built | — | 14 (10 converted C-135B, one converted EC-135C, three converted KC-135R)[source] |
|---|
| Introduction date | — | December 1965[source] |
|---|
| Developed from | — | Boeing C-135 Stratolifter[source] |
|---|
| Wing loading | — | 123.5 lb/sq ft (603 kg/m 2 )[source] |
|---|
| Thrust/weight | — | 0.21[source] |
|---|
| Country of origin | — | USA[source]Country/countries explicitly given in the equipment row Origin column; not the country operating the row. WC-135R Constant Phoenix |
|---|