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 Best viewed in
 800 x 600 screen
 resolution
 | Drawings
Click on the thumbnail image to get a larger version. 
            
                | High Resoultion
                Version |  | Low Resoultion
                Version |  
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                | Airfoil
                section |  
                | Wing | Wortmann FX 76MP - 180 (18%) at
                the root Wortmann FX 76MP - 120 (12%) at the tips
 |  
                | Tail | Initially E 193 inverted: now
                NASA 641012 |  
                | Rudder | NASA 641012 |  
                | Propeller | 24 Eppler 193 | 
 
            
                | Dimensions |  |  
                | Aircraft Weight | Initially 39 kg at 23 metres: now
                37 kg at 28 m |  
                | Wingspan | Initially 23 metres, now 28
                metres with tip extensions |  
                | Wing Area | Initially 17.5 sq metres, now 22sq metres |  
                | Wing root cord | 1.06 metres |  
                | Wing tip cord | 0.5 metres |  
                | Aspect ratio | 34:1 |  
                | Fuselage boom length | 7.85 metres |  
                | Tailplane span | 3.6 metres |  
                | Rudder Height | 2.7 metres |  
                | Propeller diameter | 3.0 metres | 
 
            
                | Construction
                Materials |  
                | Wing |  |  
                | Ribs | 6mm white foam, end ribs of each
                section 12mm blue foam. 0.5 mm hardwood veneer
                rib capstrips from TE to spar glued with PVA,
                compression brace of 12 x 6 mm balsa on both
                sides of each 3rd rib. |  
                |  |  |  
                | Leading Edge |  |  
                |  |  |  
                | Main Spar | Carbon-blue foam composite, 28 layers of
                carbon on top for compression strength, 18 layers
                on bottom for tension strength Epoxy glues in all
                spar constructions.. |  
                |  |  |  
                | Trailing Edge | Blue foam covered in some carbon fibre
                sheeting |  
                |  |  |  
                | Covering | Front-3mm blue styrofoam, Bottom rear- 1
                micron Astroll Clear mylar.Rear top- 16 mm white
                styrofoam. |  
                |  |  |  
                | Fuselage |  |  
                | Shell | Fibreglass (2 layers of 4 oz) for the cockpit
                tub shell. |  
                |  |  |  
                | Seat |  |  
                |  |  |  
                | Cranks & pedals |  |  
                |  |  |  
                | Chain |  |  
                |  |  |  
                | Boom | Prepreg (vinyl ester resin) carbon fibre
                cylinder made on a mandril, heated in an oven at
                150 degrees for 1 1/2 hrs and pressed off with
                about 2 tonnes pressure. |  
                |  |  |  
                | Clear section | Clear Mylar for the windscreen with Profilm
                to cover the rear open surfaces. |  
                |  |  |  
                | Tail |  |  
                | Radio Control | 5 cell (to allow for voltage drop),
                1700mah battery, Tartan 12 kg-cm torque, 1/4
                scale sized servos for surface control, 1 servo
                for each aileron, 1 for elevator and 2 for
                rudder. Transmitter JR MC 16. |  
                | Propeller | The propeller is hollow, balsa ribbed and
                balsa skinned, covered in 3/4 glass cloth. The 2
                propeller halves are attached to a chrome-
                molybdenium tube. |  |