Hawker Harrier
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Harrier | |
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Hawker Harrier prototype at A &AEE |
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Type | Torpedo Bomber |
Manufacturer | Hawker Aircraft Limited |
Designed by | Sydney Camm |
Maiden flight | February 1927 |
Status | Prototype |
Number built | One |
The Hawker Harrier was an experimental biplane torpedo bomber aircraft built by Hawker Aircraft to a specification issued in the 1920s for the RAF.
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[edit] Development
In 1925, the British air ministry laid down specifications for a replacement for the Hawker Horsley bomber and for a coastal torpedo bomber (Specifications 23/25 and 24/25). As these specifications were similar, the Air Ministry announced that a single competition would be held to study aircraft submitted for both specifications. [1]
Sydney Camm of Hawker Aircraft designed the Harrier to meet the requirements of Specification 23/25, with the prototype (J8325) first flying in February 1927, the first of the competitors to the two specifications to fly. [1] The Harrier was a two seater powered by a Bristol Jupiter VIII armed with one Vickers machine gun and one Lewis gun carrying either one torpedo or a maximum of 1,000 lb (~500 kg) of bombs.
The prototype Harrier was tested at the Aeroplane and Armament Experimental Establishment (A & AEE) at Martlesham Heath in November 1927, where, while it met the requirements of Specification 23/25, and had satisfactory handling, it had an inferior bombload to the Hawker Horsley, the aircraft it was meant to replace [1]. It was therefore modified to carry a torpedo. On testing the modified aircraft, however, it was found to be underpowered, being incapable of taking off with torpedo, gunner and a full fuel load[1]. It was therefore not considered further, the competition ultimately being won by the Vickers Vildebeest[1].
The prototype was used by Bristol as an engine testbed, flying with the 870 hp Bristol Hydra and the 495 hp Bristol Orion engines [1].
[edit] Specifications (Harrier (Bomber))
General characteristics
- Crew: Two
- Length: 29 ft 7 in (9.02 m)
- Wingspan: 46 ft 3 in (14.10 m)
- Height: 13 ft 4 in (4.07 m)
- Wing area: 497 ft² (46.2 m²)
- Empty weight: 3,278 lb (1,490 kg)
- Loaded weight: 5,656 lb (2,561 kg)
- Powerplant: 1× Bristol Jupiter VIII nine cyliner radial engine, 583 hp (435 kW)
Performance
- Maximum speed: 117 knots (135 mph, 217 km/h)
- Cruise speed: knots (mph, km/h)
- Range: nm (mi, km)
- Service ceiling 20,000 ft (6,100 m)
- Rate of climb: ft/min (m/s)
- Wing loading: 11.4 lb/ft² (55.4 kg/m²)
- Power/mass: 0.103 hp/lb (0.170 kW/kg)
- Climb to 10,000 ft (3050 m): 18 min 30 sec
Armament
- One forward firing Vickers gun and one Lewis gun on Scarff ring in rear cockpit.
- either one torpedo or 1,000 lb bombs
[edit] See also
Comparable aircraft
[edit] References
[edit] External links
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