| Kallithea | |
|---|---|
 | |
| Role | Autogyro |
| National origin | Bulgaria |
| Manufacturer | Niki Rotor Aviation |
| Introduction | 2011 |
| Status | In production (2017) |
| Produced | 2011-present |
| Developed from | Niki Lightning |
The Niki Kallithea (the best view) is a Bulgarian autogyro designed and produced by Niki Rotor Aviation of Pravets, introduced in 2011. The aircraft is supplied complete and ready-to-fly. [1] [2]
The Kallithea is a development of the 2009 Niki Lightning, differing mainly in its use of a conventional two-tube tail boom that passes under the pusher propeller instead of mounting the tail boom through the propeller hub.
The Kallithea features a single main rotor, a two-seats-in tandem enclosed cockpit with fold-up doors, tricycle landing gear and a four-cylinder, liquid and air-cooled, four stroke 100 hp (75 kW) Rotax 912 or six-cylinder, liquid cooled side-valve four-stroke flat six 4-litre petrol 120 hp (89 kW) D-Motor LF39 aircraft engine in pusher configuration. The doors can also be removed for flight. [1]
The aircraft fuselage is a monocoque structure made from composites and fibreglass. Its two-bladed Vortech or Sport Copter rotor has a diameter of 8.5 m (27.9 ft) and a chord of 21 cm (8.3 in). The aircraft has a typical empty weight of 250 kg (551 lb) and a gross weight of 450 kg (992 lb), giving a useful load of 200 kg (441 lb). With full fuel of 80 litres (18 imp gal; 21 US gal) the payload for the pilot, passenger and baggage is 143 kg (315 lb). [1]
Data from Tacke [1]
General characteristics
Performance
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