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Caspar C.17

Posted on June 6, 2026 By

After the departure of chief designers Ernst Heinkel and Karl Theiss from the firm Hanseatische Flugzeugwerke Karl Caspar AG, Ernst von Loessl took over as chief engineer. Alongside military aircraft development, Loessl also began designing a range of civilian aircraft.

Table of Contents

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    • Development for Competition
    • A Single Prototype
    • Technical Specifications
  • Image and diagram gallery of the Caspar C.17
    • How to cite this article:

Development for Competition

In 1924, the light aircraft Caspar C.17 was built to participate in the Deutschen Rundflug competition. It was a two-seater wooden low-wing monoplane, equipped with an ABC Scorpion engine producing 30 hp.

A Single Prototype

The unsuccessfully chosen power plant prevented the aircraft from achieving widespread recognition. Consequently, only a single example of the Caspar C.17 was ever built.

Technical Specifications

Modification C.17
Wingspan, m 12.00
Length, m 5.00
Wing area, m2 15.59
Empty weight 145
Normal takeoff weight 325
Engine type 1 Piston engine ABC Scorpion
Power, hp 1 x 30
Maximum speed, km/h 1 25
Cruising speed, km/h 105
Service ceiling, m 3500
Crew 2

Image and diagram gallery of the Caspar C.17

Caspar C.17 light aircraft
C.17
Caspar C.17 light aircraft
C.17
Caspar C.17 light aircraft
C.17
Caspar C.17 light aircraft
C.17

How to cite this article:

APA: Caspar C.17 (). Caspar C.17. wp.archivoaereo.com. https://wp.archivoaereo.com/en/caspar-c-17-2/
VANCOUVER: Caspar C.17 [online]. wp.archivoaereo.com; [cited 2026-06-15]. Available at: https://wp.archivoaereo.com/en/caspar-c-17-2/
Developed by Agatha Press
Pioneer Light Aircraft Tags:Caspar AG, Germany

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