KK-1e Utu Fibrera   

General Details
Manufacturer: Fibrera
Plane Name:

KK-1e Utu

Classified as: Unclassified
Country Of Origin: Finland
Designer: Ahto Anttila
No. of Seats 1
No. Built 22
   
Performance:
L/DMax: 35 80 kph / 43kt / 50 mph
   
MinSink: 0.61 m/s / 2.0 fps / 1.18 kt
   


 

Specifications:
Span Area Empty Weight Payload Gross Weight Wing Load Water Ballast
m ft sq.m sq.ft kg lb. kg lb. kg lb. kg
/sq.m
lb.
/sq.ft
kg lb.
15 49.2 11.24 121 200 441 110 242 310 683 27.58 5.65 0 0
Aspect ratio: 20
Airfoil: NACA 63 (3)-618 root. 63(1)-612 tip
Structure: all fiberglass (all loads taken on unispar).
Engine:

Comment:
A Standard Class sailplane which first flew in 1964, the Utu has a fixed landing wheel and a trailing-edge split spoiler/terminal-velocity brake. One surface rotates up like a spoiler and the other splits down like a flap and the resultant air deflection from the upper spoiler drives the wing down in a strong negative lift configuration.


           

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