Consolidated Vultee XP-81
The Consolidated Vultee XP-81 (later redesignated ZXF-81) is a development of the Consolidated Vultee Aircraft Corporation to build a single seat, long range escort fighter that combined use of both turbojet and turboprop engines. Although promising, the lack of suitable engines combined with the end of World War II doomed the project.
|Manufacturer||Consolidated Vultee Aircraft Corporation|
|First flight||11 February 1945|
|Primary user||United States Army Air Forces|
Design and developmentEdit
Two prototype aircraft were ordered on 11 February 1944 that were designated XP-81. The engine selection was an attempt to couple the high-speed capability of the jet engine with the endurance offered by the propeller engine. The XP-81 was designed to use the General Electric TG-100 turboprop engine (later designated XT31 by the US military) in the nose driving a four-bladed propeller and a GE J33 turbojet in the rear fuselage. The turboprop would be used for normal flight and cruising and the turbojet added for high-speed flight.
The first XP-81 (serial 44-91000) was completed in January 1945 but because of developmental problems the turboprop engine was not ready for installation. A decision was then made to mount a complete V-1650-7 engine package from a P-51D aircraft in place of the turboprop for initial flight tests. This was done in a week and the Merlin-powered XP-81 was sent to the Muroc airbase where it flew for the first time on 11 February 1945. During 10 flight test hours, the XP-81 displayed good handling characteristics except for inadequate directional stability due to the longer forward portion of the fuselage (this was rectified by enlarging the vertical tail).
While 13 YP-81 pre-production aircraft had been ordered, the capture of Guam and Saipan eliminated the need for long-range, high-speed escort fighters and then, just before VJ Day the contract was cancelled, after 85% of the engineering was completed. The YP-81 was to be essentially the same as the prototype but with a lighter and more powerful GE TG-110 (XT41) turboprop engine, the wing moved aft 10 inches (0.25 m), and armament of either six .50 cal (12.7 mm) machine guns or six 20 mm cannon.
After the XP-81 was returned to Vultee Field, the TG-100 turboprop was installed and flight testing resumed, including the first flight by an American turboprop-powered aircraft on 21 December 1945. However, the turboprop engine was not able to produce its designed power; producing only the same output as the Merlin (1,490 hp or 1112 kW) with the resultant performance limited to that of the Merlin-engined version.
- United States Army Air Forces (testing only)
Note: Performance is estimated with "full powered" TG-100. Armament is projected only.
- Crew: 1
- Length: 44 ft 8 in (13.61 m)
- Wingspan: 50 ft 6 in (15.39 m)
- Height: 13 ft 6 in (4.11 m)
- Wing area: 425 sq ft (39.5 m2)
- Empty weight: 12,979 lb (5,887 kg)
- Gross weight: 24,650 lb (11,181 kg)
- Powerplant: 1 × General Electric T31-GE-3 turboprop engine, 2,300 shp (1,700 kW) plus 600 lbf (2.7 kN) residual thrust (estimated power of production engine)
- Powerplant: 1 × General Electric J33-GE-5 centrifugal flow turbojet, 3,750 lbf (16.7 kN) thrust (planned engine for production aircraft)
- Propellers: 4-bladed constant-speed propeller, 12 ft (3.7 m) diameter
- Maximum speed: 478 mph (769 km/h, 415 kn) at sea level; 507 mph (816 km/h) at 30,000 ft (9,100 m)
- Cruise speed: 275 mph (443 km/h, 239 kn) at 30,000 ft (9,100 m)
- Range: 2,500 mi (4,000 km, 2,200 nmi)
- Service ceiling: 47,000 ft (14,000 m)
- Rate of climb: 5,300 ft/min (27 m/s)
- Wing loading: 106 lb/sq ft (520 kg/m2)
Aircraft of comparable role, configuration, and era
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