Mü 25

The Mü25 was designed as a high performance single-seater for aerodynamical tests. Its projected steel framework fuselage should be aerodynamical enhanced by fibre composite fairings. The The Mü25 was not finished.

Wing span 17m
Wing area 16.5m²
Profile STE 861-615
Empty weight 230kp
Max. weight 360kp
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