Credit
颐园居 · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
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Measured figures
Configuration
| Specification | Hongdu GJ-11 | Lihiniya MK I |
|---|---|---|
| Crew | None[source] | — |
| Type | Unmanned combat aerial vehicle Loyal wingman drone[source] | Unmanned aerial vehicle[source] |
| National origin | People's Republic of China[source] | Sri Lanka[source] |
| Manufacturer | Hongdu Aviation Industry Group[source] | Sri Lanka Air Force Centre for Research and Development[source] |
Wingspan
Single source14.4 m (47 ft 3 in)[source]
Maximum take-off; Max takeoff weight
Single source115 lb (52 kg)[source]
Maximum; For Phase 1
Single source60 kn (69 mph, 110 km/h) For Phase 1[source]
1 × Hirth 4103 two-stroke, air cooled, opposed engine
Single source1 × Hirth 4103 two-stroke, air cooled, opposed engine, 8 hp (6.0 kW)[source]
Service ceiling
Single source10,000 ft (3,000 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] | Sri Lanka Air Force[source] |
|---|
| First flight | November 2013[source] | — |
|---|
| Powerplant | 1 × unnamed Guizhou -built turbofan[source] | — |
|---|
| Developed into | — | Lihiniya MK II[source] |
|---|
| Fuel capacity | — | 19 liter[source] |
|---|