Wingspan : 1700 mm .Wing area 30.23 sq.dm ;
Airfoil stabilizer : NACA -0008. Tailplane area: 4.95 sq.dm .
Total surface area : 35.18 sq.dm ;
Fuselage length : 1070 ii ;
Fuselage : sandwich : glas-carbon ( weight of 420 gr.)
Wing : sandwich glass-carbon-balsa-glass ( spar-sp.carbon)-
weight of 650 gr.
Stabilizer : sandwich glass-balsa-glass (weight of 58 gr.)
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