Wikiwand AI

Paramania Vortex

From Wikipedia, the free encyclopedia

National originFrance, United Kingdom
Designer
Mike Campbell-Jones
Vortex
General information
TypeParamotor
National originFrance, United Kingdom
ManufacturerParamania LLC
Designer
Mike Campbell-Jones
StatusProduction completed
History
Introduction date2002

The Paramania Vortex is a French/British paramotor that was designed by Mike Campbell-Jones and produced by Paramania of Le Chillou, France and later of London, England for powered paragliding. Introduced about 2002 and now out of production, when it was available the aircraft was supplied complete and ready-to-fly.[1]

The Vortex was designed to comply with the US FAR 103 Ultralight Vehicles rules as well as European regulations. It features a paraglider-style wing, single-place accommodation and a single engine in pusher configuration with a reduction drive and a diameter two-bladed composite propeller. The engine and propeller used varies by model. The fuel tank capacity is 10 litres (2.2 imp gal; 2.6 US gal). Early wings used in 2002 included the Paramania Reflex, while this was later developed into the Paramania Action wing by 2004.[1]

As is the case with all paramotors, take-off and landing is accomplished by foot. Inflight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw.[1]

Variants

Specifications (Vortex Solo)

References

Related Articles

Timelines

Top Qs

Fact Checks