Blériot XXXIII
In 1912, Louis Blériot constructed the unusual Blériot XXXIII, a two-seater mid-wing monoplane featuring a canard configuration. This innovative aircraft was initially powered by a 70-horsepower Gnome engine. Its maiden flight took place in June 1912, though it unfortunately concluded with a minor accident.
Initial Design and Flight
Following the incident, the Blériot XXXIII underwent significant restoration. The landing gear was redesigned to improve stability and functionality. Furthermore, the aircraft received a power upgrade with the installation of a new Gnome engine, this time boasting 80 horsepower, aimed at optimizing its overall performance.
Technical Specifications
The Blériot XXXIII’s specifications included a wingspan of 10.50 meters and a length of 8.00 meters. It featured a wing area of 24.00 m² and a normal takeoff weight of 330 kg. The aircraft achieved a maximum speed of 115 km/h and accommodated a crew of two, making it suitable for various early aviation purposes.
Technical Specifications
| Modification | Blériot XXXIII |
| Wingspan, m | 10. 50 |
| Length, m | 8. 00 |
| Wing area, m2 | 24.00 |
| Normal takeoff weight | 330 |
| Engine type | 1 Piston engine Gnome |
| Power, hp | 1 x 790 |
| Maximum speed, km/h | 115 |
| Crew | 2 |
Image and diagram gallery of the Blériot XXXIII
 Blériot XXXIII |
 Blériot XXXIII |
 Blériot XXXIII |
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