Engineering:Pivot-Koechlin monoplane
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Short description: 1910s French aircraft
Pivot-Koechlin monoplane | |
---|---|
Role | Observation aircraft |
National origin | France |
Manufacturer | Pivot and Paul Koechlin |
First flight | 1911 |
Number built | 1 |
The Pivot-Koechlin monoplane was a French experimental monoplane aircraft built in the early 1910s.
Specifications
General characteristics
- Crew: 3
- Length: 7.80 m (25 ft 7 in)
- Wingspan: 10.00 m (32 ft 10 in)
- Wing area: 17.00 m2 (183.0 sq ft)
- Powerplant: 1 × Gnome 7 Omega 7-cylinder air-cooled rotary piston engine, 37 kW (50 hp)
- Propellers: 2-bladed fixed-pitch propeller
Performance
- Maximum speed: 110 km/h (68 mph, 59 kn)
References
Original source: https://en.wikipedia.org/wiki/Pivot-Koechlin monoplane.
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