| Built as a private venture, the Heron single-seat fighter
was noteworthy in that it was the first of the Hawker
company's fighters to have a predominantly metal
structure. A single-bay biplane with provision for two
7.7mm synchronised Vickers guns, the
Heron was built up of round steel and aluminium tubing
bolted together (rather than welded) and braced by
high-tensile wires. The result was a light and easily reparable
structure, but it was perhaps the novelty of its
construction rather than any shortcomings in capability
that militated against service adoption. This was
despite the fact that the prototype, initially flown early
in 1925, was highly praised during official trials at Martlesham
Heath in 1926. The prototype was subsequently
returned to the manufacturer by which it was
flown until mid-1928.
 | A three-view drawing (600 x 438) |
WEIGHTS |
Take-off weight | 1418 kg | 3126 lb |
Empty weight | 962 kg | 2121 lb |
DIMENSIONS |
Wingspan | 9.70 m | 32 ft 10 in |
Length | 6.78 m | 22 ft 3 in |
Height | 2.97 m | 10 ft 9 in |
Wing area | 27.03 m2 | 290.95 sq ft |
PERFORMANCE |
Max. speed | 251 km/h | 156 mph |
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