Credit
VoidWanderer · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
Measured figures
Maximum take-off; Max takeoff weight
Single source15 kg (33 lb)[source]
Configuration
| Specification | DeViRo Leleka-100 | STC Orlan-10 |
|---|---|---|
| Length | — | Длина, м 1,80[source] |
| Wingspan | — | Размах крыла, м 3,10[source] |
| Type | Reconnaissance UAV[source] | Reconnaissance unmanned aerial vehicle[source] |
| National origin | Ukraine[source] | Russia[source] |
| Manufacturer | DeViRo |
Maximum; Maximum speed
Single source150 km/h (93 mph, 81 kn)[source]
Ferry; Ferry range
Single source600 km (370 mi, 320 nmi)[source]
Combat range
Single source110 km (68 mi, 59 nmi)[source]
1 × Saito Manufacturing FA-62B single-cylinder four-stroke glow fuel piston engine
Single source1 × Saito Manufacturing FA-62B single-cylinder four-stroke glow fuel piston engine , 0.71 kW (0.95 hp)[source]
Service ceiling
Single source5,000 m (16,000 ft)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Special Technology Center (STC)[source] |
| Primary user | Armed Forces of Ukraine[source] | — |
|---|
| Introduction date | 2015[source] | — |
|---|
| Alternative designation | Leleka-100[source] | — |
|---|
| Status | — | In service[source] |
|---|
| Primary users | — | Russian Ground Forces Ministry of Emergency Situations[source] |
|---|
| Capacity | — | 6 kg (13 lb) payload[source] |
|---|
| Launch method | — | folding catapult platform[source] |
|---|
| Landing method | — | parachute recovery[source] |
|---|
| Max. wind speed at launch | — | 10 m/s[source] |
|---|
| Operational temperature range | — | −30 to +40 °C[source] |
|---|
| Optical imaging | — | Canon EOS 750D / EOS 800D digital SLR camera with EF 85mm f/1.8 USM lens[source] |
|---|
| Thermal imaging | — | TM2005016-F19 Lynred PICO640gen2 infrared camera[source] |
|---|
| Reported operators | — |
|
|---|