Hanriot H.26
1923
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Hanriot H.26

Designed to compete in the 1921 CI (single-seat fighter) programme, the H.26 was the only participant powered by the 260hp Salmson 9Z nine-cylinder radial engine. Most other contenders were intended for the water-cooled inline HS 8F. The H.26 design attempted to compensate for lower installed power by means of aerodynamic cleanliness. It was a sesquiplane of all-metal construction with metal skinning on the wing leading edges and forward fuselage, the remainder being fabric covered. The H.26 employed thick aerofoil sections, the upper wing being faired into the oval-section fuselage, and it had a close-cowled engine with a large propeller spinner. First flown at Orly in 1923, the H.26 utilised a Botali radiator arranged in a semi-circle behind the engine. As this was found to provide insufficient cooling, two Chausson radiators were attached to the undercarriage strutting. The H.26 displayed poor handling qualities, which, coupled with continued engine overheating and an inadequate view offered the pilot, led to the abandonment of further development after several test flights.

Hanriot H.26


Specification 
 MODELH.26 (estimated)
 WEIGHTS
    Take-off weight1150 kg2535 lb
    Empty weight820 kg1808 lb
 DIMENSIONS
    Wingspan9.05 m30 ft 8 in
    Length7.35 m24 ft 1 in
    Height2.50 m8 ft 2 in
    Wing area18.00 m2193.75 sq ft
 PERFORMANCE
    Max. speed260 km/h162 mph
    Ceiling8500 m27900 ft
    Range750 km466 miles

3-View 
Hanriot H.26A three-view drawing (1670 x 1213)

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