| Horizon AIR S-100 UAV
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| takeoff weight | up to 200 kg
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| maximum payload weight | 50 kg
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| operating height range: static ceiling – up to 3500 m
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| dynamic ceiling | up to 4500 m
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| speed range | up to 200 km / h
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| flight duration | at least 6 hours
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| return flight range | at least 250 km
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| placement of payload equipment (compartment volume and allowable payload mass)
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| main compartment | 13175 cm3, payload weight, up to 50 kg
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| bow compartment | 6460 cm3, payload weight, up to 10 kg
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| compartment of auxiliary electronic equipment | 15000 cm3, weight payload up to 10 kg
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| side supports | payload, up to 10 kg on each side.
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| Lmax | 4010mm (157.87")
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| fuselage length | 3110mm,
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| fuselage height (max) | 708 mm
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| fuselage width (max) | 500 mm
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| full height to propeller hub | 1118 mm
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| ground clearance | 343 mm
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| track | 1240 mm
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| diameter main rotor | 3400 mm,
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| tail rotor diameter | 660 mm,
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| length stabilizer | 500 mm.
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| original dry weight (in ex. condition) | ~110 kg,
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| take-off weight max | 200 kg
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| amount of fuel | 41 l
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| mass of filled oil | 1.75 l
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| mass of the payload | up to 50 kg
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| Static ceiling | 3050 m (140 kg), 2070 m (160 kg), 1250 m (180 kg), 850 m (200 kg)
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| Dynamic ceiling | 4572 m
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| With lightweight flight weight V max (design restrictions) | 240 km/h.
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| V cruising max | 185 km/h.
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| V patrol for max flight duration | 102 km/h.
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| V patrols for a maximum flight range of 120 km / h.
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| Vertical V hover climb: | 5 m/s
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| manual mode, control (RRU) | 3 m/s in automatic mode (ARC)
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| Vertical V climb and descent in flight: | 1m/s AGC, RRU.
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