The Blériot-SPAD S.XXI was a prototype fighter built by SPAD in the late 1910s, derived from the SPAD S.XIII. The specification lists a crew of one, a length of 6.40 m, a wingspan of 8.43 m, a height of 2.41 m, a wing area of 23.5 square metres, an empty weight of 750 kg, a gross weight of 1,048 kg, a maximum speed of 221 km/h and a service ceiling of 7,000 m from one 220 kW Hispano-Suiza 8Fb V-shaped eight-cylinder inline engine. Its armament was two fixed forward-firing synchronised 7.7 mm Vickers machine guns.
Facts
Top Speed (km/h) Maximum Mass (kg) Connections
Derived From
Source Blériot-SPAD S.XXI (Wikipedia)
Exemplifies
Source Blériot-SPAD S.XXI (Wikipedia)
Of Make
Source Blériot-SPAD S.XXI (Wikipedia)
In the Other Atlases
Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source Blériot-SPAD S.XXI (Wikipedia)LeadQuote, Lead
The Blériot-SPAD S.XXI was a prototype fighter plane built by SPAD in the late 1910s
Sources
1. Blériot-SPAD S.XXI (Wikipedia)
Specifications
Empty weight: 750 kg (1,653 lb)
Specifications, maximum mass
Gross weight: 1,048 kg (2,310 lb)
Specifications, top speed
Maximum speed: 221 km/h (137 mph, 119 kn)
Specifications, powerplant
220 kW (300 hp)
Lead
The Blériot-SPAD S.XXI was a prototype fighter plane built by SPAD in the late 1910s
View the SourceReader Challenges (0)
No disputes yet. Spotted an error or a better source? Open the first one.
Sign in to dispute this or suggest a correction.