Celier Kiss Explained

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.[1]

Design and development

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.

Variants

Kiss 582
  • A proposed single seat variant under development in 2011. It will be powered by the twin cylinder, liquid-cooled, two-stroke, dual-ignition 640NaN0 Rotax 582 engine. The cockpit will be either partially or, optionally, fully enclosed.
    Kiss 912
  • Base model, with two seats in tandem, powered by a four cylinder, air and liquid-cooled, four-stroke, dual-ignition 800NaN0 Rotax 912UL engine in pusher configuration. The cockpit has a semi-enclosed fairing with a windshield.
    Kiss 912S
  • Upgraded model, with two seats in tandem, powered by a four cylinder, air and liquid-cooled, four-stroke, dual-ignition 1000NaN0 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 four cylinder, air and liquid-cooled, four-stroke, dual-ignition 1150NaN0 Rotax 914 engine in pusher configuration. The cockpit has a fully enclosed fairing.

    Notes and References

    1. Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 178. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X