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Celier Kiss
 
 Celier-Kiss
 
The Celier Kiss is a series of Polish autogyros that was designed by Frenchman Raphael Celier and produced by his company, Celier Aviation of Jaktorów-Kolonia, Poland. When it was available the aircraft was supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.
 
The tandem seat Kiss series was designed as a complement to the side-by-side configuration Celier Xenon 2 series of autogyros. The Kiss series all feature a single main rotor, tricycle landing gear, a low-set T-tail and a choice of engines, all mounted in pusher configuration.
 
In 2011 the Kiss 912, assembled, cost €29,900.
 
Variants:
 
Kiss 912
Base model, with two seats in tandem, powered by a 80 hp (60 kW) Rotax 912UL engine in pusher configuration. The cockpit has a semi-enclosed fairing with a windshield.
Main rotor diameter: 8.4 m (27 ft 7 in)
Main rotor area: 55.4 m2 (596 sq ft)
Empty weight: 200 kg (441 lb)
Gross weight: 450 kg (992 lb)
Fuel capacity: 50 litres (11 imp gal; 13 US gal)
Maximum speed: 140 km/h (87 mph, 76 kn)
Endurance: 3 hours
Rate of climb: 3 m/s (590 ft/min)
Disk loading: 8.1 kg/m2 (1.7 lb/sq ft)
Crew: one
Capacity: one passenger
 
Kiss 912S
Upgraded model, with two seats in tandem, powered by a 100 hp (75 kW) Rotax 912ULS engine in pusher configuration. The cockpit has a fully enclosed fairing.
 
Kiss 914
Turbocharged model, with two seats in tandem, powered by a 115 hp (86 kW) Rotax 914 engine in pusher configuration. The cockpit has a fully enclosed fairing.
 
 
 
 
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