Historical P-51 Mustang

Last updated

P-51 Mustang
116th Fighter Squadron - P-51 Mustangs.jpg
Role Homebuilt aircraft
National origin United States
Manufacturer Historical Aircraft Corporation
StatusProduction completed
Developed from North American P-51 Mustang

The Historical P-51 Mustang is an American homebuilt aircraft that was designed and produced by the Historical Aircraft Corporation of Nucla, Colorado. The aircraft is a 62.5% scale replica of the original North American P-51 Mustang and when it was available was supplied as a kit for amateur construction. [1]

Contents

Design and development

The aircraft features a cantilever low-wing, a single-seat enclosed cockpit under a bubble canopy, retractable conventional landing gear and a single engine in tractor configuration. [1]

The aircraft is made from welded steel tubing covered in a shell of polyurethane foam and fiberglass. Its 24.00 ft (7.3 m) span wing, mounts flaps and has a wing area of 100.00 sq ft (9.290 m2). The cockpit width is 21 in (53 cm). The standard engine used is the 230 hp (172 kW) Ford Motor Company V-6 automotive conversion powerplant. [1]

The aircraft has a typical empty weight of 1,354 lb (614 kg) and a gross weight of 1,954 lb (886 kg), giving a useful load of 600 lb (270 kg). With full fuel of 41 U.S. gallons (160 L; 34 imp gal) the payload for pilot and baggage is 354 lb (161 kg). [1]

The aircraft has fairly lengthy runway requirements with a standard day sea level take-off distance of 1,200 ft (366 m) and a landing distance of 1,500 ft (457 m). [1]

The kit included prefabricated assemblies, the engine and scale fixed pitch propeller, instruments and avionics. The manufacturer estimated the construction time from the supplied kit as 2000 hours. [1]

Specifications (P-51)

Data from AeroCrafter [1]

General characteristics

Performance

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References

  1. 1 2 3 4 5 6 7 Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 177. BAI Communications, 15 July 1998. ISBN   0-9636409-4-1