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Caspar C.33

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Caspar C.33

Aircraft Development and Design

In 1928, Caspar Werke AG constructed a training aircraft, which was designated Caspar C.33. It was a two-seat biplane, equipped with a five-cylinder, air-cooled Armstrong-Siddeley Mongoose engine, producing 135 hp.

Market Reception and Fate

The C.33 failed to interest the military. An attempt to sell it to private customers as a sports plane was also unsuccessful. Consequently, the aircraft remained a single prototype.

Technical Specifications

Modification C.33
Wingspan, m 8.00
Length, m 5.30
Empty weight 490
Maximum takeoff weight 750
Engine type 1 Piston engine Armstrong-Siddeley Mongoose
Power, hp 1 x 135
Maximum speed, km/h 160
Cruising speed, km/h 130
Crew, crew members 2

Image and diagram gallery of the Caspar C.33

C.33 training aircraft
C.33
C.33 training aircraft
C.33

Caspar Werke AGGerman

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Caspar C.33 • wp.archivoaereo.com — Aerial Archive