Credit
颐园居 · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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At a glance
Measured figures
Length
Single source12.2 m (40 ft 0 in)[source]
CQ-10A · Length
Single sourceConfiguration
| Specification | Hongdu GJ-11 | MMIST CQ-10 SnowGoose |
|---|---|---|
| Crew | None[source] | — |
| Type | Unmanned combat aerial vehicle Loyal wingman drone[source] | Unmanned Aerial Vehicle (UAV)[source] |
| National origin | People's Republic of China[source] | Canada[source] |
| Manufacturer | Hongdu Aviation Industry Group[source] | MMIST[source] |
9.5 ft (2.9 m)[source]
Gross; CQ-10A · Gross weight
Single source1,400 lb (635 kg)[source]
Maximum; CQ-10A · Maximum speed
Single source38 mph (61 km/h, 33 kn)[source]
CQ-10A · Range
Single source180 mi (300 km, 160 nmi)[source]
CQ-10A · 1 × Rotax 914 UL piston engine
Single source1 × Rotax 914 UL piston engine, 110 hp (82 kW)[source]
CQ-10A · Maximum
Single sourceCQ-10A · with 200 lb cargo
Single source19 hr (Maximum), 9-11 hr with 200 lb cargo[source]
CQ-10A · Service ceiling
Single source18,000 ft (5,500 m)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer |
|---|
Shenyang Aircraft Design Institute Hongdu Aviation Industry Group Aviation Industry Corporation of China[source] |
| — |
| Status | In development[source] | — |
|---|
| Primary user | People's Liberation Army Air Force[source] | United States Special Operations Command[source] |
|---|
| First flight | November 2013[source] | April 2001[source] |
|---|
| Powerplant | 1 × unnamed Guizhou -built turbofan[source] | — |
|---|
| Number built | — | CQ-10A: 15 (49 planned)[source] |
|---|
| Introduction date | — | January 2005[source] |
|---|
| Capacity | — | 575 pounds (261 kg)[source] |
|---|
| Fuel capacity | — | 91 U.S. gallons (340 L)[source] |
|---|
| Reported operators | — |
|
|---|