Blériot XXI
Blériot Aéronautique · France · first flew 1911 · reconnaissance aircraft
The Blériot XXI was an early French reconnaissance monoplane, developed from the Blériot XI-2 and XIV.
Recognition (WEFT)
| W — Wings | High-mounted, straight |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | 8.31 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Shoulder-wing monoplane with wing-warping lateral control
- Pilot and observer seated side by side
- Single 70 hp Gnome Gamma rotary engine driving a two-bladed propeller
A shoulder-wing monoplane with a rotary engine, a shallow tapering fuselage and Blériot-style sprung undercarriage with a cross-bar below the fuselage.
Specifications
- The Blériot XXI has a length of 8.31 m (27 ft).
- It has a wingspan of 11.15 m (37 ft).
- Its maximum speed is 95 km/h (59 mph).
- Typical crew: 2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
It first flew in February 1911. The rectangular fuselage tapered to a horizontal knife-edge at the tail.
Variants
It was developed from the Type XI-2 and XIV. No variants are listed.
Where you'll see it
A Type XXI was one of two Blériot designs entered in the 1912 British Military Aeroplane Competition.
Related aircraft
- Blériot XII
- Blériot 117
- Blériot 155
- Blériot 165
- Gotha Taube LE-3
- Nieuport VI
- REP Type N
- Royal Aircraft Factory B.E.2
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