The
is a two seat, all composite aircraft desgined to
comply with B.C.A.R. Section "S" of the
British regulations for microlight group aircraft.
The basic structure is
assembled from extruded polystyrene with some
plywood components (e.g. the wing mainspar). The
foam structure is encapsulated in woven glass
cloth and epoxy resin.
The power plant is a BMW 1000cc
'boxer' engine.
An 'all flying' canard with a NACA 0012 symmetrical
aerofoil setion is used for maximum efficiency.
Seating is tandem with the passeneger close to the
centre of gravity.
Wing section is NACA 4412, tapered and swept c/w
anti-vortex tops.
Ailerons are differentialised (1:1.5), large area,
small deflection.
is a two seat, all composite aircraft desgined to
comply with B.C.A.R. Section "S" of the
British regulations for microlight group aircraft.
