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AutoGyro Calidus vs NIKI Rotor Aviation Lightning

Published specifications side by side. Every figure comes from the manufacturer, with the date it was last checked on each model page.

AutoGyro Calidus and NIKI Rotor Aviation Lightning compared on published specifications.
Specification AutoGyro Calidus NIKI Rotor Aviation Lightning
Cruise speed 90 to 185 km/h (55 to 115mph) 135 km/ h
Empty mass 300 kg (660 lbs) 285 kg
Engine Rotax 912 ULS | 914 UL | 915 iS | 916 iS Rotax 912 ULS/ 914 UL
Fuel capacity 74 L to 100 L (19.5 to 26.4 US gallons) 70 Liter (18.5 US gallons)
Height 2.8 m (9.1 ft) 2850 mm
Length 4.8 m (15.66 ft) 4550 mm
Mtom 500 to 560 kg (1100 to 1235 lbs) 560 kg
Range Up to 600 km (373 miles) Endurance 4 h with 30 min reserve
Rotor diameter 8.4 m | 8.6 m | 8.8 m (27.3 ft | 27.95 ft | 28.6 ft) 8,5 m
Seats Two-seat tandem model Not published
Takeoff roll 70 to 110 m (230 to 361 ft) 0-150 m
Vne 225 km/h (140 mph) 180 km
Engine power Not published 100 hp
Propeller Not published Composite

11 of 14 specifications are published by both manufacturers. A blank is a figure the manufacturer does not publish, not a zero and not a weakness. Verify anything that matters against the flight manual before you buy.