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Schmeidler SN.2

Technische Hochschule Breslau · Germany · Interwar (1919–1938)

Schmeidler SN.2 — Fixed Wing
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The Schmeidler SN.2 was a low power, single seat aircraft designed in Germany in the 1930s to test the ability of trailing edge wing extensions to lower minimum flight speeds without a high speed drag penalty.

Specifications

Category
Fixed Wing
Domain
Civil
Era
Interwar (1919–1938)
Country
Germany
Manufacturer
Technische Hochschule Breslau
Service Entry
1932
Produced
1
Engine
1× five cylinder radial
Length (ft)
20
Wingspan (ft)
37
Empty Weight (lb)
783
MTOW (lb)
1036
Endurance (hr)
2 hours
Service Ceiling (ft)
9613
Range (mi)
186
Max Speed (mph)
99