Republic XP-72

XP-72

Role: Fighter
Manufacturer: Republic Aviation Company
First flight: 2 February 1944
Status: Cancelled
Number built: 2
Developed from: Republic P-47

The Republic XP-72 was an American prototype interceptor fighter developed as a progression of the P-47 Thunderbolt design. The XP-72 was designed around the Pratt & Whitney R-4360 twenty-eight cylinder radial air-cooled engine with a supercharger mounted behind the pilot and driven by an extension shaft from the engine. The armament consisted of six 0.5 in wing-mounted machine guns and underwing racks for two 1,000 lb bombs.

Design and development

The XP-72 development paralleled that of another Republic design, the XP-69 that was to be powered by an experimental forty-two cylinder Wright R-2160 radial engine mounted behind the pilot and driving contra-rotating propellers through an extension shaft. The XP-69 was intended for high altitude operations and featured a pressurized cockpit and armament of two 37 mm cannon and four 0.5 in machine guns. As the XP-72 displayed greater promise than the XP-69, the XP-69 was canceled on 11 May 1943 and an order for two XP-72 prototypes was placed on 18 June 1943.

Operational history

The XP-72 flew for the first time on 2 February 1944, equipped with a four bladed propeller. The second prototype was completed on 26 June 1944 and was equipped with an Aero-Products contra-rotating propeller. As the XP-72 displayed exceptional performance during flight tests an order for 100 production aircraft was awarded. The order included an alternate armament configuration of four 37 mm cannon. By this time the war had progressed to where the need was for long-range escort fighters and not high-speed interceptors. Also, the advent of the new turbojet-powered interceptors showed greater promise for the interceptor role. Thus, the production order for the P-72 was cancelled.

Specifications (XP-72)

General characteristics

Crew: One
Length: 36 ft 7 in (11.15 m)
Wingspan: 40 ft 11 in (12.47 m)
Height: 16 ft (4.88 m)
Wing area: 300 ft² (27.9 m²)
Empty weight: 11,476 lb (5,216 kg)
Loaded weight: 14,433 lb (6,560 kg)
Max takeoff weight: 17,490 lb (7,950 kg)
Powerplant: 1x— Pratt & Whitney R-4360-13 radial engine, 3,000 hp @ sea level (dash 13 engine) (2,574 kW)

Performance

Maximum speed: 480 mph (789 km/h at sea level)
Range: 1,200 miles (1,932 km)
Service ceiling: 42,000 ft (12,805 m)
Rate of climb: 5,280 ft/min (26.8 m/s)
Wing loading: 48.1 lb/ft² (235 kg/m²)
Power/mass: 0.24 hp/lb (0.39 kW/kg)

Armament

6x— 0.50 in Browning machine guns
2x— 1,000 lb (476 kg) bombs

Related development

P-47 Thunderbolt

Citations

Bibliography

Bodie, Warren. "The Whine of the Jug". Wings Magazine (Vol. 4, No. 4), August 1974, p. 33-39.
Freeman, Roger A. Thunderbolt: A Documentary History of the Republic P-47. London: Macdonald & Jane's (Publishers) Ltd., 1978. ISBN 0-354-01166-9.
Green, William. War Planes of the Second World War - Fighters (Volume Four). London: Macdonald & Co.(Publishers) Ltd., 1961. ISBN 0-356-01448-7.
Green, William and Gordon Swanborough. WW2 Aircraft Fact Files: US Army Air Force Fighters, Part 2. London: Macdonald & Jane's (Publishers) Ltd., 1978. ISBN 0-354-01072-7.
Jarski, Adam and Robert Michulec. P-47 Thunderbolt, P-35/P-43/XP-72 (Monografie Lotnicze 26) (in Polish). Gdynia: AJ-Press, 1996. ISBN 83-86208-41-4.

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Source: WikiPedia