Credit
Baiweiflight · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Measured figures
Wing Loong I · Length
Single source9.05 m (29 ft 8 in)[source]
RQ-170 · Length
Single sourceConfiguration
| Specification | CAIG Wing Loong | Lockheed Martin RQ-170 Sentinel |
|---|---|---|
| Type | MALE UCAV[source] | Unmanned aerial vehicle (UAV)[source] |
| Manufacturer | Chengdu Aircraft Industry Group[source] | Lockheed Martin[source] |
| Designer | Chengdu Aircraft Design Institute[source] | — |
| Status | in service & in production[source] | In service[source] |
14 ft 9 in (4.5 m)[source]
Gross; Wing Loong I · Gross weight
Single source1,100 kg (2,425 lb)[source]
Maximum; Wing Loong I · Maximum speed
Single source280 km/h (170 mph, 150 kn)[source]
Wing Loong I · Range
Single source4,000 km (2,500 mi, 2,200 nmi)[source]
Wing Loong I · 1 × Rotax 914 turbocharged 100 shp
Single source1 × Rotax 914 turbocharged, 75 kW (100 shp)[source]
Wing Loong I · of air-to-surface weapons
Single source200 kilograms (440 lb) of air-to-surface weapons[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| 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] | 2007[source] |
|---|
| First flight | 2009[source] | — |
|---|
| Developed into | CAIG Wing Loong II[source] | Shahed 171 Simorgh Shahed Saeqeh[source] |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Country of origin | People's Republic of China[source] | — |
|---|
| Primary user | — | United States Air Force[source] |
|---|
| Number built | — | 20 to 30[source] |
|---|
| Powerplant | — | 1 × Garrett TFE731 or General Electric TF34 turbofan[source] |
|---|
| National origin | — | United States[source] |
|---|
| Reported operators |
| — |
|---|