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At a glance
Measured figures
Length
Single source4 ft 7 in (1.4 m)[source]
Wing Loong I · Length
Single sourceConfiguration
| Specification | AeroVironment RQ-20 Puma | CAIG Wing Loong |
|---|---|---|
| Crew | — | None (UAV)[source] |
| Type | Miniature UAV[source] | MALE UCAV[source] |
| Manufacturer | AeroVironment[source] | Chengdu Aircraft Industry Group[source] |
| Primary users | United States Army United States Marine Corps United States Air Force Albanian Air Force[source] | People's Liberation Army Air Force Egyptian Air Force United Arab Emirates Air Force Pakistan Air Force[source] |
9.05 m (29 ft 8 in)[source]
Wing Loong I · Height
Single source2.77 m (9 ft 1 in)[source]
Wing Loong I · 1 × Rotax 914 turbocharged 100 shp
Single source1 × Rotax 914 turbocharged, 75 kW (100 shp)[source]
Wing Loong I · Service ceiling
Single source5,000 m (16,000 ft)[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.
| Number built | + 1,000[source] | — |
|---|
| Introduction date | 2008[source] | 2011[source] |
|---|
| First flight | 2007[source] | 2009[source] |
|---|
| Minimum control speed | 23 mph (37 km/h, 20 kn)[source] | — |
|---|
| National origin | United States[source] | — |
|---|
| Designer | — | Chengdu Aircraft Design Institute[source] |
|---|
| Status | — | in service & in production[source] |
|---|
| Manufactured | — | 2009[source] |
|---|
| Developed into | — | CAIG Wing Loong II[source] |
|---|
| Propellers | — | 3-bladed[source] |
|---|
| Country of origin | — | People's Republic of China[source] |
|---|
| Reported operators | — |
|
|---|