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Ligero civil

Che-15

2 min read
Che-15

Design and Development of the Che-15

The Che-15 is a light two-seater aircraft designed by Boris Chernov. This prototype was manufactured and tested at the facilities of the Experimental Design Bureau of Light Aviation (OKB-LA). Its design focused on simplicity and adaptability for various aerial functions.

Key Features and Adaptability

This versatile aircraft boasts a dual-control system and interchangeable landing gear, allowing for float, wheel, or ski configurations to suit any surface. Furthermore, its open cockpit and the ability to fold its wings for transport make it a practical and easy-to-handle option.

Versatile Applications

Thanks to its innovative features, the Che-15 serves as an ideal means of transport for training and practice flights. It is also perfectly suited for tourist and recreational activities, offering a unique and accessible flying experience.

Technical Specifications

Modification Che-15
Wingspan, m 9.08
Aircraft length, m 7.03
Aircraft height, m 2.05
Wing area, m2 12.10
Empty weight 250
Maximum takeoff weight 480
Engine type 1 Piston engine Rotax 582-2V
Power, hp 1 x 64
Maximum speed, km/h 120
Cruising speed, km/h 100
Practical range, km 250
Max. operational overload 4
Crew 1-2
Payload up to 2 passengers

Image gallery of the Che-15

OKB LARussian
Che-15 • wp.archivoaereo.com — Aerial Archive