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ModificationOrlan-10
| | type | aircraft, large high wing
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| Wingspan, m | 3.10
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| Length, m | 1.80
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| Height, m |
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| Weight, kg empty | 12.50
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| Takeoff weight | 14 kg (some models 18-20 kg)
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| Payload | up to 5 kg (previously up to 2.5 kg)
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| Weight/payload | 4 (previously 6, up to 5/3 kg)
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| Power plant | One internal combustion engine on gasoline A95
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| Non-stop flight time | up to 10 hours (according to other sources up to 960 minutes)
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| Power, hp | 1 x
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| speed, km/h | 70-150 km/h
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| cruising Speed | 80 km/h
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| Practical range, km | up to 600 km in autonomous mode
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| Range | 500-1000 km (according to various sources); as part of the Leer-3 complex up to 120 km.
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| Max. range of application | up to 120/100 km from the ground control station
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| Communication range | up to 100 km with ground antenna
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| Flight duration, h | 10-18 [or 16/10 hour]
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| Ceiling | up to 6000 meters (according to other sources up to 5000 meters) above sea level
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| Takeoff | from a collapsible catapult
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| Maximum allowable wind speed at the start | 10 m/s
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| Operating temperature range at the ground surface | from minus 30 to plus 40 degrees Celsius
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| Landing | parachute
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| Features | In one flight, it can survey an area of up to 500 sq. km.
The Leer-3 complex is based on the KamAZ-5350 chassis.
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