|First flight||10 March 1937|
|Primary user||Royal Air Force|
Design and development
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Fairey, Gloster and Hawker attempted to fulfil this need and competition was tight to attain the highest performance possible. As the aircraft required only a modest bomb load and with performance being paramount, the Hawker design team chose to focus its efforts on developing an aircraft similar in size to their Hurricane fighter.
The Hurricane was then in an advanced design stage and there would be economies of scale if some assemblies were common to both aircraft. This resulted in the Henley, as it was to become known, sharing identical outer wing panel and tailplane jigs with the Hurricane. Both were equipped with the Rolls-Royce Merlin engine as it offered the best power-weight ratio as well as a minimal frontal area. The Henley’s cantilever fabric-covered monoplane wing was mid-set, a retractable tail wheel landing gear was selected and accommodation provided for a pilot and observer/air gunner, which differed from the Hurricane’s single-seat cockpit.
Although construction of a Henley prototype began as early as mid-1935, with priority given to Hurricane development, it was not until 10 March 1937 that, powered by a Merlin "F" engine, it was first flown at Brooklands, shortly after the competing Fairey P.4/34. Subsequently, the aircraft was refitted with light alloy stressed-skin wings and a Merlin I engine (production version of the F) and further test flights confirmed the excellence of its performance. It could reach a top speed of 300 mph (480 km/h).
However, at this point the Air Ministry had by this point decided that it no longer required a light bomber (probably because this role was felt to be adequately filled by the Fairey Battle). Accordingly, the Henley, which in line with RAF policy had not been fitted with dive brakes; bomb crutches; or specialised bomb sights and thus limited to attack angles of no greater than 70° (and consequently far less accurate than specialised German dive bombers of the same period, notably the Ju 87 Stuka, fitted with all of the foregoing and a semi-automatic bomb release and dive termination system and thus capable of near-vertical dives of pin-point accuracy) was relegated to target-towing duty.
Henley production was subcontracted to Gloster Aircraft and 200 were ordered into production.
The second prototype was fitted with a propeller-driven winch to haul in drogue cable after air-to-air firing sorties. This was first flown on 26 May 1938.
Production Henley III aircraft, entered service with Nos. 1, 5 and 10 Bombing and Gunnery Schools, as well as with the Air Gunnery Schools at Barrow, Millom and Squires Gate. Unfortunately, it was soon discovered that unless the aircraft were restricted to an unrealistically low towing speed of 220 mph (350 km/h), the rate of engine failures was unacceptably high, attributed to a cooling system matched to the Henley's original missions but inadequate when towing a target at high engine speed but low airspeed. Henleys were relegated to towing larger drogue targets with anti-aircraft co-operation units, predictably proving themselves even less well-suited to this role; the number of engine failures increased and problems with engines were compounded by difficulties releasing drogue targets. Several Henleys were lost after the engine cut out and the drogue could not be released quickly enough. A solution was never found to this problem and in mid-1942, the Henley was withdrawn from service, in favour of adapted Boulton Paul Defiants and specialised Miles Martinet aircraft.
- Henley I
- Henley II
- Second prototype.
- Henley III
- Two-seat target tug aircraft for the RAF, 200 built.
- Hawker Hotspur
- Prototype two seater fighter variant of the Henley with a four-gun power-driven turret. This did not reach production, the requirement being met by the Defiant.
- Royal Air Force
Specifications (Henley Mk III)
- Crew: 2
- Length: 36 ft 5 in (11.10 m)
- Wingspan: 47 ft 10½ in (14.59 m)
- Height: 14 ft 7½ in (4.46 m)
- Wing area: 342 ft² (31.77 m²)
- Empty weight: 6,010 lb (2,726 kg)
- Max. takeoff weight: 8,840 lb (3,846 kg)
- Powerplant: 1 × Rolls-Royce Merlin II inline piston engine, 1,030 hp (768 kW)
- Maximum speed: (with drogue) 272 mph at 17,500 ft (438 km/h at 5,300 m)
- Cruise speed: 235 mph at 15,000 ft (378 km/h at 4,500 m)
- Range: 950 mi (1,529 km)
- Service ceiling: 27,000 ft (8,200 m)
- Rate of climb: 1,150 ft/min (340 m/min)
- Wing loading: 25.9 lb/ft² (121 kg/m²)
- Power/mass: 0.121 hp/lb (0.200 kW/kg)
Aircraft of comparable role, configuration and era
- Cooper, H.J.,O.G. Thetford and C.B. Maycock. Aircraft of the Fighting Powers - Volume II. Leicester, UK: Harborough Publishing, 1942.
- Gunston, Bill. Classic World War II Aircraft Cutaways. London: Osprey, 1995. ISBN 1-85532-526-8.
- Hannah, Donald. Hawker FlyPast Reference Library. Stamford, Lincolnshire, UK: Key Publishing Ltd., 1982. ISBN 0-946219-01-X.
- James, Derek N. Hawker, an Aircraft Album No. 5. New York: Arco Publishing Company, 1973. ISBN 0-668-02699-5. (First published in the UK by Ian Allan in 1972)
- Mason, Francis K. Hawker Aircraft since 1920. London: Putnam, 1991. ISBN 0-85177-839-9.
- Mondey, David. The Hamyln Concise guide to British aircraft of World War II. London: Hamlyn/Aerospace, 1982. ISBN 0-600-34951-9.
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