Origin and Purpose
In 1925, the light sport aircraft Caspar C.23 was constructed by Caspar Werke AG to participate in the Deutschen Rundflug competition. This model was specifically designed for the sport aviation sector, aiming to combine performance with lightweight construction.
Technical Specifications
The Caspar C.23 was a two-seater high-wing monoplane, powered by a 100 hp (74 kW) Mercedes D.I engine. This aircraft was produced as a single example, receiving the registration number D-648, making it a unique piece in aviation history.
Technical Specifications
| Modification | C.23 |
| Wingspan, m | 10.00 |
| Length, m | 7.00 |
| Empty weight | 480 |
| Normal takeoff weight | 730 |
| Engine type | 1 Piston engine Mercedes D.I |
| Power, hp | 1 x 100 |
| Maximum speed, km/h | 150 |
| Cruising speed, km/h | 135 |
| Crew, crew members | 2 |
Image and diagram gallery of the Caspar C.23
 C.23 |
How to cite this article:
APA: Caspar C.23 (). Caspar C.23. wp.archivoaereo.com. https://wp.archivoaereo.com/en/caspar-c-23-2/
VANCOUVER: Caspar C.23 [online]. wp.archivoaereo.com; [cited 2026-07-30]. Available at: https://wp.archivoaereo.com/en/caspar-c-23-2/