Armstrong Whitworth F.K.10

Length
6.7056 m
Flat Wing Span
8.2296 m
Height
3.3528 m
Flat Wing Area
36.2693 m²
Max Speed
135.1849 km/h
Max Ceiling
3048 m
Number of Engines
1
Aircraft Engine
First Flight
1916-01-01
Number Built
9

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All data (19 fields)
Name
Armstrong Whitworth F.K.10
Manufacturer
Armstrong Whitworth
Description
The Armstrong Whitworth F.K.10 was a British two-seat quadruplane (i.e., four wing) fighter aircraft built by Armstrong Whitworth during the First World War.
First Flight
1916-01-01
Designer
Frederick Koolhoven
Type
Fighter
Length (m)
6.7056
Height (m)
3.3528
Max Speed (km/h)
135.1849
Max Ceiling (m)
3048
Armament
1 × fixed, forward-firing .303 in (7.7 mm) Vickers machine gun and 1 × .303 in (7.7 mm) Lewis Gun in observer's cockpit
Endurance (h)
2
Number Built
9
Powerplant Description
1 × Clerget 9B nine-cylinder rotary engine, 97 kW (130 hp) each
Wikipedia Article (URL)
en.wikipedia.org/wiki/Armstrong_Whitworth_F.K.10
Flat Wing Span (m)
8.2296
Flat Wing Area (m²)
36.2693
Aircraft Engine
Clerget 9B
Number of Engines
1