An advanced two-seat man-powered aircraft completed by the Southend Man-Powered Aircraft Group, UK. The pilots were located in the nose, side-by-side, beneath a fully enclosed cockpit. A tractor propellor was mounted above the pilots. The fuselage was circular section, with conventional tail surfaces at the extreme rear. A high mounted wing had considerable taper to the tips. The construction was metal tube with balsa non-load carrying parts. The covering was aluminium foil. Tricycle undercarriage.
The project was abandoned after early tests showed mechanical drive problems.
Wingspan: 90.00 ft
Wing area: 400 sq.ft
Aspect ratio: 20:1
Empty weight: 156 lb
All Aero 