Engineering:Blériot XLII
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Short description: WWI French reconnaissance aircraft
| Blériot XLII | |
|---|---|
| General information | |
| Type | Reconnaissance |
| National origin | France |
| Manufacturer | Blériot |
| Number built | 1 |
| History | |
| First flight | March 1913 |
The Blériot XLII was a First World War French reconnaissance plane designed and built by Blériot.
Design
The crew was housed in a partially armored cabin. A small window was installed in front of the fuselage to facilitate observation. For reconnaissance, the observer lay horizontally on the cabin floor.[1]
Development
The Bleriot XLII was built in March 1913 for use as a reconnaissance and observation aircraft. It was a double mid-flight, equipped with an 80 hp Gnome engine. The Bleriot XLII passed the test cycle, but the military was not interested.
Specifications
Data from Aviafrtance : Blériot XLII [2]
General characteristics
- Crew: 2
- Length: 7.30 m (23 ft 11 in)
- Wingspan: 8.50 m (27 ft 11 in)
- Wing area: 18.00 m2 (193.8 sq ft)
- Powerplant: 1 × Gnome Monosoupape 7 Type A air-cooled rotary piston engine, 60 kW (80 hp)
- Propellers: 2-bladed fixed-pitch propellers
Performance
References
- ↑ "Bleriot XLII". https://www.airwar.ru/enc/other1/bleriotxlii.html.
- ↑ Parmentier, Bruno. "Blériot XLII" (in French). Paris. https://www.aviafrance.com/aviafrance1.php?ID=10061&ID_CONSTRUCTEUR=212&ANNEE=0&ID_MISSION=0&MOTCLEF=. Retrieved 24 January 2019.
Template:Louis Blériot aircraft
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