Credit
w:United States Navy photo by Mass Communication Specialist 3rd Class Kenneth G. Takada · Public domain · Resized · Public domain · Source ↗ · Modified
FORCETALLY
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Measured figures
Configuration
| Specification | Honeywell RQ-16 T-Hawk | Hongdu GJ-11 |
|---|---|---|
| Crew | None[source] | None[source] |
| Type | Surveillance UAV[source] | Unmanned combat aerial vehicle Loyal wingman drone[source] |
| National origin | United States[source] | People's Republic of China[source] |
| Manufacturer | Honeywell[source] | Hongdu Aviation Industry Group |
Wingspan
Single source14.4 m (47 ft 3 in)[source]
Gross; approximate · Gross weight
Single source18.5 lb (8.39 kg)[source]
Maximum; approximate · Maximum speed
Single source81 mph (130 km/h, 70 kn)[source]
approximate · 1 × 3W-Modellmotoren 3W-56 56cc Boxer Twin piston engine
Single source1 × 3W-Modellmotoren 3W-56 56cc Boxer Twin piston engine , 4 hp (3 kW)[source]
approximate · Endurance
Single source40 minutes[source]
approximate · Service ceiling
Single source10,500 ft (3,200 m)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Primary user | United States Army[source] | People's Liberation Army Air Force[source] |
|---|
| Fuel capacity | 2.1 lb (0.95 kg)[source] | — |
|---|
| Operational altitude | 100-200 ft (30-70 m)[source] | — |
|---|
| Designer | — | Shenyang Aircraft Design Institute Hongdu Aviation Industry Group Aviation Industry Corporation of China[source] |
|---|
| Status | — | In development[source] |
|---|
| First flight | — | November 2013[source] |
|---|
| Powerplant | — | 1 × unnamed Guizhou -built turbofan[source] |
|---|