Engineering:Curtiss XP-22 Hawk
| XP-22 Hawk | |
|---|---|
| |
| Role | Experimental biplane fighter |
| Manufacturer | Curtiss Aeroplane and Motor Company |
| Primary user | United States Army Air Forces |
| Number built | 1 |
| Variants | Curtiss P-6 Hawk |
The Curtiss XP-22 Hawk was a 1930s United States experimental biplane fighter built by Curtiss for evaluation by the United States Army Air Service.
Design and development
In 1929, the AAC ordered three P-11 Hawks for testing of the 600 hp (447 kW) H-1640 Chieftain engine. This engine proved a failure, and before completion, one of the three was converted to use a 9-cylinder 575 hp (429 kW) Cyclone, being completed as the YP-20. Testing with the R-1820 was prolonged, so the Army acquired another of the three P-11s, instead. This became the XP-22.
A number of changes were made for installing the 700 hp (520 kW) Curtiss V-1570 Conqueror engine. The radiator was relocated, a new cowl was fitted, and the tail was given more fin and less rudder area, and featured a steerable tailwheel, rather than the original skid. For these changes, Curtiss charged only US$1.[1]
During testing, the XP-22 underwent a number of alterations and improvements, including a change from a three-strut landing gear to a single streamlined strut, later fitted with wheel pants. Fillets were added where struts joined the wing and the tail was briefly reduced in area, to P-6 standard.[1] The XP-22 was also the Army's first fighter capable of 200 mph (320 km/h), achieving 202 mph (325 km/h).[2]
Operational history
In June 1931, the AAC held a competition to evaluate the P-6, P-12, YP-20, and XP-22. The XP-22 came out the winner, earning a contract for 45 aircraft as the Y1P-22. Following the trials, the XP-22 donated a nose and landing gear graft to the YP-20, which became the XP-6E, and the 45 production aircraft were completed to this standard.
Operators
United States
Specifications (XP-22 Hawk)
Data from U.S.Fighters,[2] Curtiss Aircraft 1907–1947[3]
General characteristics
- Crew: 1
- Length: 23 ft 7 in (7.19 m)
- Wingspan: 31 ft 6 in (9.60 m)
- Height: 8 ft 10 in (2.69 m)
- Airfoil: Clark Y[4]
- Empty weight: 2,597 lb (1,178 kg)
- Max takeoff weight: 3,354 lb (1,521 kg)
- Powerplant: 1 × Curtiss V-1570-23 Conqueror V-12 water-cooled piston engine, 575 hp (429 kW)
- Propellers: 2-bladed propeller
Performance
- Maximum speed: 202 mph (325 km/h, 176 kn)
- Service ceiling: 26,500 ft (8,100 m)
Armament
- Guns: 2x 0.300 in (7.62 mm) machine-guns in the fuselage sides
References
- ↑ 1.0 1.1 Fitzsimons 1978, p. 1255.
- ↑ 2.0 2.1 Jones 1975, p. 58.
- ↑ Bowers, Peter M. (1979). Curtiss aircraft, 1907-1947. London: Putnam. p. 262. ISBN 0370100298.
- ↑ Lednicer, David. "The Incomplete Guide to Airfoil Usage". https://m-selig.ae.illinois.edu/ads/aircraft.html.
Further reading
- Donald, David, ed. Encyclopedia of World Aircraft. Etobicoke, Ontario, Canada: Prospero Books, 1997. ISBN:1-85605-375-X.
- Fitzsimons, Bernard, ed. "Hawk, Curtiss Models 34 and 35 P-1 to P-6 and F6C". Illustrated Encyclopedia of Weapons and Warfare. Volume 12, pp. 1255–1256, London: Phoebus Publishing, 1978.
- Jones, Lloyd S. U.S. Fighters: 1925-1980s. Fallbrook, California: Aero Publishers, Inc., 1975. ISBN:0-8168-9200-8.
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