|HD.3 C.2 and HD.4|
|First flight||June 1917|
|Primary users||Aéronautique Militaire
|Number built||ca. 90|
The Hanriot HD.3 C.2 was a two-seat fighter aircraft produced in France during World War I.
Design and development
Similar in appearance to a scaled-up HD.1, the Hanriot HD.3 was a conventional, single-bay biplane with staggered wings of equal span. The pilot and gunner sat in tandem, open cockpits and the main units of the fixed tailskid undercarriage were linked by a cross-axle. Short struts braced the fuselage sides to the lower wing.
Flight testing revealed excellent performance, and the French government ordered 300 of the type in 1918, in preparation for a major offensive the following year. When the war ended, the contract was cancelled with around 75 aircraft having been delivered to the Aéronautique Militaire and at least 15 to the Aéronautique Maritime. One example was delivered to the Aéronautique Maritime in summer 1918 equipped with twin float undercarriage and a larger tailfin; it was intended that this would be the prototype of a dedicated floatplane fighter designated HD.4, but the war ended before any further development took place. The Armistice also led to the abandonment of a dedicated night fighter variant, the HD.3bis, with enlarged and balanced ailerons and rudder and with a wing of increased section.
- HD.3 C.2
Main production version
- HD.3bis CN.2
- Nightfighter prototype with thick wing section and revised control surfaces (1 built)
- Floatplane derivative of HD.3. One built.
- HD.9 Ap.1
- Single-seat photo-reconnaissance biplane, powered by a 260 hp (194 kW) Salmson 9Za radial piston engine. Ten evaluation aircraft were ordered, with the first completed in November 1918.
Specifications (HD.3 C.2)
Data from War Planes of the First World War
- Crew: Two, pilot and gunner
- Length: 6.95 m (22 ft 9 1⁄2 in)
- Wingspan: 9.00 m (29 ft 6 1⁄4 in)
- Height: 3.00 m (9 ft 10 in)
- Wing area: 25.5 m2 (274.5 ft2)
- Empty weight: 760 kg (1,670 lb)
- Gross weight: 1,180 kg (2,611 lb)
- Powerplant: 1 × Salmson 9Za nine-cylinder water-cooled radial engine, 195 kW (260 hp) each
- Maximum speed: 192 km/h (119 mph)
- Range: 498 km (310 miles)
- Endurance: 2 hours
- Service ceiling: 5,700 m (18,700 ft)
- Rate of climb: 4.1 m/s (800 ft/min)
- Taylor and Alexander 1969, pp. 94-95.
- Bruce 1972, p. 21.
- Bruce 1972, p. 19.
- Bruce 1972, pp. 32–35.
- Bruce 1971, p. 22.
- at 2,000 m (6,600 ft)
- 3 min 21 s to 1,000 m (3,300 ft)
|Wikimedia Commons has media related to Hanriot HD.3.|
- Bruce, J.M. War Planes of the First World War: Volume Five, Fighters. London: Macdonald, 1972. ISBN 0-356-03779-7.
- Taylor, John W. R. and Jean Alexander. Combat Aircraft of the World. New York: G.P. Putnam's Sons, 1969. ISBN 0-71810-564-8.
- Taylor, Michael J. H. Jane's Encyclopedia of Aviation. London: Studio Editions, 1989. ISBN 0-517-69186-8.
- World Aircraft Information Files. London: Bright Star Publishing, File 896 Sheet 11.
- S, W (January–February 2012). "Rara Avis - The Hanriot HD.3.C2". Windsock Worldwide. Albatros Productions. 28 (1): 15–18.