JDM Roitelet
| JDM Roitelet | |
|---|---|
| Type: | Light aircraft |
| Design country: | |
| Manufacturer: |
Avions JDM |
| First flight: |
January 3, 1949 |
The Roitelet (French for wren ) was a light aircraft made by the French manufacturer Avions JDM .
description
The low wing was a wooden structure with plywood planking. The cantilever wing had flaps. The landing gear had a tail spur. The open cockpit was just above the trailing edge of the wing. Since no suitable engine could be found for series production, only a prototype was completed. After development was discontinued, the company was dissolved.
Technical specifications
| Parameter | Data |
|---|---|
| span | 6.95 m |
| length | 4.15 m |
| Wing area | 6.10 m² |
| Empty mass | 105 kg |
| Max. Takeoff mass | 210 kg |
| Top speed | 155 km / h |
| Flight duration | 2 hours 30 minutes |
| Engine | a piston engine with 25 HP (18.6 kW) |
literature
- AERO, issue 16, page 446