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 gallery of the Caspar C.33