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bielik jet
 
"MALGOSIA"
experimental

TECHNICAL DATA :

Span : 14.0 m

Lenght : 8.0 m

Wing area : 12.34 m2

Wing aspect ratio : 15.88

Wing airfoil : NACA 641412

Tail area : 1.873 m2

Tail airfoil : NACA 631012 - 63006 mod.

Vertical empennage area : 1.123 m2

Vertical empennage airfoil : NACA 632015 - 631012

Weight empty max. : 490 kG

Weight,max in flight : 700 kG

 

 

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