Republic XP-72
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P-72 | |
---|---|
Type | Fighter |
Manufacturer | Republic Aviation Company |
Maiden flight | 2 February 1944 |
Status | Cancelled |
Number built | 2 |
The Republic XP-72 was a 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 turbo-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 under wing racks for two 1,000 lb bombs.
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 machineguns. 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.
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.
[edit] 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: 1× Pratt & Whitney R-4360-13 radial engine, 3,450 hp (2,574 kW)
Performance
- Maximum speed: 490 mph at 25,000 ft (789 km/h)
- 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
[edit] Reference
- Green, William. War Planes of the Second World War - Fighters (Vol 4). London: Macdonald, 1961.
[edit] Related content
Related development
Comparable aircraft
XP-69
Designation sequence
XP-69 - P-70 - XP-71 - XP-72
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