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.
Specifications
General Characteristics
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- Wingspan 37.1ft (11.3m)
- Length 32.6ft (9.9m)
- Height 12.7ft (3.9m)
- Empty Weight 8,825lbs (4,002kg)
- Loaded Weight 13,597lbs (6,167kg)
Performance
- Power/Weight Ratio 0.826
- Horse Power/Weight Ratio 0.073
- Wing Loading 51.1lbs/ft2 (249.5kg/m2)
- Wing Area 266.1ft2 (24.7m2)
- Drag Points 3935
Parts
- Number of Parts 52
- Control Surfaces 5
- Performance Cost 265
