Credit
Baiweiflight · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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At a glance
Measured figures
Wing Loong I · Length
Single source9.05 m (29 ft 8 in)[source]
X-47B · Length
Single sourceConfiguration
| Specification | CAIG Wing Loong | Northrop Grumman X-47B |
|---|---|---|
| Crew | None (UAV)[source] | None aboard (semi-autonomous operation)[source] |
| Type | MALE UCAV[source] | Unmanned combat aerial vehicle Technology demonstrator[source] |
| Manufacturer | Chengdu Aircraft Industry Group[source] | Northrop Grumman[source] |
| Designer | Chengdu Aircraft Design Institute[source] | — |
38 ft 2 in (11.63 m)[source]
Wing Loong I · 1 × Rotax 914 turbocharged 100 shp
Single source1 × Rotax 914 turbocharged, 75 kW (100 shp)[source]
Wing Loong I · Endurance
Single source20 hours[source]
Wing Loong I · of air-to-surface weapons
Single source200 kilograms (440 lb) of air-to-surface weapons[source]
X-47B · Wing area
Single source953.6 sq ft (88.59 m 2 )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Status | in service & in production[source] | Active[source] |
|---|
| Primary users | People's Liberation Army Air Force Egyptian Air Force United Arab Emirates Air Force Pakistan Air Force[source] | — |
|---|
| Manufactured | 2009[source] | — |
|---|
| Introduction date | 2011[source] | — |
|---|
| First flight | 2009[source] | 4 February 2011[source] |
|---|
| Developed into | CAIG Wing Loong II[source] | — |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Country of origin | People's Republic of China[source] | — |
|---|
| National origin | — | United States[source] |
|---|
| Primary user | — | United States Navy[source] |
|---|
| Number built | — |
|---|
| Developed from | — | Northrop Grumman X-47A Pegasus[source] |
|---|
| Powerplant | — | 1 × Pratt & Whitney F100-220U turbofan[source] |
|---|
| Reported operators |
| — |
|---|