Operating Life: 1981
UAS Locaxtion: Hangar 1
Maximum Speed: 75mph
Cruise Speed: 65mph
Engine: Robin EC34PM, 30hp
Rate of Climb: 750ft/min
Wing Span: 30ft
Range: 220 miles
Fuel Tank Capacity: 22.7 Litres
Single-seated, single-engined, mid-wing monoplane with conventional three-axis control. Wing has swept back leading and trailing edges, and tapering chord; no tail, canard wing. Pitch control by elevator on canard; yaw control by tip rudders; roll control by half-span up-only ailerons and spoilers; control inputs through stick for pitch/roll and pedals for yaw.
Cantilever wing; main-wing profile, modified Liebeck; canard profile, GU25; both double-surface. Undercarriage has three wheels in tricycle formation; no suspension on nosewheel and glass-fibre suspension on main wheels. Push-right go-right nosewheel steering connected to yaw control. No brakes.
Aluminium-tube glassfibre fuselage, partially enclosed. Engine mounted above wing driving pusher propeller.
Composite-construction wing of foam and aluminium covered with glass-fibre skin.
Image: MARK J. CAIRNS