Last site update: 03-10-2008

 

         

 

  

 

North American P-51 Mustang

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North American P-51 Mustang

North American Aviation originally designed the Mustang in response to a British specification. They agreed to produce the first prototype only 4 months after signing the contract in April 1940. The NA-73X prototype was produced in record time, but did not fly until October 26, 1940. By the end of 1941 North American had delivered the first Mustang to England for test flights. These first Mustangs were powered by the Allison V-1710 engine, a good engine, but one which didn't operate well at high altitudes.

Significant design changes came about when the Rolls-Royce Merlin V-12 was used in the P-51B/C and then when the bubble canopy P-51D/K was introduced. The P-51D Mustang was the most produced model and was favored among most pilots. The P-51H was a redesigned lighter-weight version but entered service to late to make an impact on WWII. The P-51H is noticably different in design and uses less than ten percent of the parts from the P-51D. Another light-weight, the P-51G prototypes were produced and tested. Other models, like the P-51L, P-51M never made it to production becuase the war ended.

  • P-51A,    310 built at Inglewood, California.
  • P-51B,    650 built at Inglewood.
  • P-51C,    3.750 built at Dallas, Texas.
  • P-51D/K, 6.502 built at Inglewood; 1.454 at Dallas; 200 by CAC at Fisherman's Bend, Australia. A total of 8.156.
  • P-51H,    555 built at Inglewood.

 

 

 

          P-51D

Developing Nation:

United States.

First Flight(s):

October 26, 1940.

Crew:

1.

Wing Span:

11.27 m.

Wing:

21.66 mē.

Length:

9.84 m.

Weight empty:

3.232 Kg.

Fuel and Load

Internal Fuel: 1.018 liters. (696 lit. in wings, 322 lit. in fuselage).

External Fuel: Brackets for two 284, 416 or 409 liters fuel-tanks.

Max. Weapon load: 908 Kg.

Weight Max. Load:

5.262 Kg. (including two external fuel tanks of 409 liters.

Engine (s):

Packard build Merlin V-1650-7, water cooled reversed V 12 cylinder Line engine with a two gear and two-faze turbo

(max. 1.094 KW.)

Max. Speed:

(clean) on 1.500 meters: 636 Km/h.

(clean) on 4.572 meters: 665 Km/h.

(clean) on .7620 meters: 703 Km/h.

Max. cruising speed: 583 Km/h.

Max. Height:

12.771 Meters.

Max. Range:

(clean) 1.529 Km. at 1.529 meters, at max. cruising speed.

(clean) including two external fuel tanks of 409 liters on 7.620 meters at max. cruising speed: 2.655 Km.

Operational action radius with max. fuel load: 2.092 Km.

Weapons:

- six in wing placed 12,7 mm Colt Browning M2         Machineguns with a total of 2080 shots.

- Brackets for two 227 Kg. or 454 Kg. free fall bombs.

- Bazooka like launch pipes for six 114 mm M8 detonate      rockets or six 127 mm high speed aircraft rockets launched from launch brackets under the wings.

 

 

 

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