Information
The North American Aviation P-51 Mustang is an American long-range, single-seat fighter and fighter-bomber used during World War II and the Korean War, among other conflicts. The Mustang was designed in April 1940 by a team headed by James H. Kindelberger of North American Aviation (NAA) in response to a requirement of the British Purchasing Commission. The commission approached NAA to build Curtiss P-40 fighters under license for the Royal Air Force (RAF). Rather than build an old design from another company, NAA proposed the design and production of a more modern fighter. The prototype NA-73X airframe was rolled out on 9 September 1940, 102 days after the contract was signed, and first flew on 26 October. The Mustang was designed to use the Allison V-1710 engine without an export-sensitive turbosupercharger or a multi-stage supercharger, resulting in limited high-altitude performance. The aircraft was first flown operationally and very successfully by the RAF and as a tactical-reconnaissance aircraft and fighter-bomber (Mustang Mk I). In mid 1942, Rolls Royce replaced the Allison with a Rolls-Royce Merlin 65, two-stage intercooled supercharged engine, resulting in a series of development aircraft known as the Mustang X. During testing at Hucknall, it quickly became clear that this dramatically improved the aircraft's performance at altitudes above 15,000 ft (4,600 m) (without sacrificing range). Following receipt of the test results and after further flights by a number of USAAF pilots, the results were so positive that North American began work on converting several aircraft and these were developed into the P-51B/C (Mustang Mk III) model, which became the first long range fighter to be able to compete with the Luftwaffe's fighters
Specifications
- Speed: 703 km/h (437 mph) at 7,620m (25,000 ft)
- Users: United States, United Kingdom, Canada, Australia, and others
- Type: Fighter / Bomber Escort
- RCS: Larger than modern jets (exact value unknown)
- Crew: 1
- Height: 4.17m
- Length: 9.83m
- Supercruise: Not applicable (propeller-driven aircraft)
- G limits: +8.0 (estimated)
- Radar: None (Relied on optical gunsight)