Credit
Baiweiflight · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Measured figures
Wing Loong I · Length
Single source9.05 m (29 ft 8 in)[source]
CQ-10A · Length
Single sourceConfiguration
| Specification | CAIG Wing Loong | MMIST CQ-10 SnowGoose |
|---|---|---|
| Crew | None (UAV)[source] | — |
| Type | MALE UCAV[source] | Unmanned Aerial Vehicle (UAV)[source] |
| Manufacturer | Chengdu Aircraft Industry Group[source] | MMIST[source] |
| Designer | Chengdu Aircraft Design Institute[source] | — |
| Status | in service & in production[source] |
9.5 ft (2.9 m)[source]
Wing Loong I · Height
Single source2.77 m (9 ft 1 in)[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] | January 2005[source] |
|---|
| First flight | 2009[source] | April 2001[source] |
|---|
| Developed into | CAIG Wing Loong II[source] | — |
|---|
| Propellers | 3-bladed[source] | — |
|---|
| Country of origin | People's Republic of China[source] | — |
|---|
| National origin | — | Canada[source] |
|---|
| Primary user | — | United States Special Operations Command[source] |
|---|
| Number built | — | CQ-10A: 15 (49 planned)[source] |
|---|
| Capacity | — | 575 pounds (261 kg)[source] |
|---|
| Fuel capacity | — | 91 U.S. gallons (340 L)[source] |
|---|
| Reported operators |
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