The two XP-51Bs were a more thorough conversion than the Mustang X, with a tailor-made engine installation and a complete redesign of the radiator duct. The airframe itself was strengthened, with the fuselage and engine mount area receiving more formers because of the 355 lb (161 kg) greater weight of the Packard V-1650-3 compared with the V-1710. The engine cowling was completely redesigned to house the Packard Merlin, which, because of the intercooler radiator mounted on the supercharger casing, was 5 in (130 mm) taller and used an updraft carburetor, rather than the downdraft variety of the Allison. The new engine drove a four-bladed 11 ft 2 in (3.40 m)-diameter Hamilton Standard propeller that featured cuffs of hard molded rubber. To cater for the increased cooling requirements of the Merlin, a new fuselage duct was designed. This housed a larger radiator, which incorporated a section for the supercharger coolant, and, forward of this and slightly lower, an oil cooler was housed in a secondary duct which drew air through the main opening and exhausted via a separate exit flap.
Specifications
General Characteristics
- Predecessor NorthAmerikan_P-51C-10
- Created On Android
- Wingspan 36.5ft (11.1m)
- Length 31.9ft (9.7m)
- Height 12.3ft (3.8m)
- Empty Weight 7,023lbs (3,185kg)
- Loaded Weight 8,795lbs (3,989kg)
Performance
- Horse Power/Weight Ratio 0.164
- Wing Loading 23.4lbs/ft2 (114.4kg/m2)
- Wing Area 375.4ft2 (34.9m2)
- Drag Points 630
Parts
- Number of Parts 249
- Control Surfaces 9
- Performance Cost 1,043