ArchivoAéreo

Blériot XLII

1 min de lectura
Blériot XLII

Design and Development

In March 1913, Louis Blériot constructed the Blériot XLII, a reconnaissance and observation aircraft featuring a “canard” aerodynamic scheme. This two-seater mid-wing monoplane was equipped with an 80 hp Gnome engine.

Features and Observation Role

The crew was accommodated in a partially armored cockpit. A small window was installed at the front of the fuselage to facilitate observation. For reconnaissance missions, the observer would lie horizontally on the cockpit floor, providing a better vantage point.

Testing and Outcome

The Blériot XLII underwent a series of tests. Despite its innovative design and specific features, the aircraft ultimately failed to generate interest from the military.

Technical Specifications

Modification Bleriot XLII
Wingspan, m 8. 50
Length, m 7. 30
Wing area, m2 18.00
Engine type 1 Piston engine Gnome
Power, hp 1 x 80
Crew 2

Image and diagram gallery of the Blériot XLII

Bleriot XLII
Bleriot XLII
Bleriot XLII
Bleriot XLII
Bleriot XLII
Bleriot XLII

France

Equipo Editorial de ArchivoAéreo

Grupo de investigadores y entusiastas de la aviación dedicados a documentar y preservar la historia aeronáutica mundial. Todos los artículos son revisados para garantizar precisión histórica.

Fuentes y Rigurosidad

La información presentada en esta ficha técnica ha sido compilada a partir de manuales de vuelo desclasificados, archivos históricos y bibliografía especializada. Aunque nos esforzamos por mantener la máxima precisión, algunos datos de rendimiento pueden variar según la variante específica o las condiciones operativas.