Mü10 ‘Milan’ (1934)
The "Milan" is one of the best designs  from the Akaflieger. Dipl-Ing. Egon Scheibe used steel for the first time for the fuselage. This concept was called later the 'Münchner Schule'. The wingprofile was developed by the Akaflieger. Optimized for low speed  that is thermal flights. The maximum speed is given as 290 km/h in the Air worthiness Certificate. The after seat was reached through a small hatch under the left wing. The sinking speed was 0.7 m/s as a two-seater. ( As a single seat 0.65 m/s) . It was used for many cross country flights
- 1934 Hesselberg - Praha
- 1937 Salzburg - Fara dÁlpago (Italy) 195 km
-1938 Bern - Pallanza/Lago Maggiore 136 km
It won the 1934 Rhön-Konstruktionspreis and in 1937 First prize in altitude , 2980 m, at the ISTUS-meeting. Later the aircraft was exhibited at the Deutschen Museum and survived WW 2. It was after the war used again by the new established Akaflieger in 1951 and used in the fifties. Today it is back at the Deutschen Museum
Details
Span 17.8 m
Wingarea 20 m2
Aspectratio 15.6
Wingloading 16.8 kg/m2
Wingprofile  Mü
Weight empty 180 kg
Flying weight  335 kg