North American P-51A Mustang

Fighter
VI tier

An early model of one of the most famous U.S. Army Air Force fighters of World War II. Used mainly in North Africa, Burma, and Great Britain.

  • Crew: 1
    Pilot
  • Price: 887,000
  • Research price: 25,000

Configuration North American P-51A Mustang

Engine
V
0
Engine V-1710-39
Specifications:
Engine Type water-cooled
Weight , kg 590.0
Power 1100
V
V-1710-39
VI
4900
Engine V-1710-81
Specifications:
Engine Type water-cooled
Weight , kg 600.0
Power 1200
Price:
Research price 4,900
Purchase price 55,400
VI
4900
V-1710-81
VI
6500
Engine V-1650-1
Specifications:
Engine Type water-cooled
Weight , kg 720.0
Power 1300
Price:
Research price 6,500
Purchase price 57,000
VI
6500
V-1650-1
VII
11500
Engine V-1650-3
Specifications:
Engine Type water-cooled
Weight , kg 730.0
Power 1490
Price:
Research price 11,500
Purchase price 60,300
VII
11500
V-1650-3
Airframe
V
0
Airframe P-51
Specifications:
Weight , kg 2940.0
Hit Points 250
V
P-51
VI
7200
Airframe P-51A
Specifications:
Weight , kg 2960.0
Hit Points 275
Price:
Research price 7,200
Purchase price 65,000
VI
7200
P-51A
Wing-mounted weapon
VI
0
Machine gun 12.7 mm AN/M2 (W)
Ineffective against armored targets
Specifications:
Weight , kg 76.0
Caliber , mm 12.70
Rate of Fire , rounds/min 750
Muzzle Velocity , m/s 890
Damage 78
VI Ineffective against armored targets
4x12.7 mm AN/M2 (W)
VII
15800
Machine gun 12.7 mm MG-53-2 (W)
Ineffective against armored targets
Specifications:
Weight , kg 78.0
Caliber , mm 12.70
Rate of Fire , rounds/min 850
Muzzle Velocity , m/s 890
Damage 89
Price:
Research price 15,800
Purchase price 24,500
VII Ineffective against armored targets
15800
4x12.7 mm MG-53-2 (W)

Specifications

Hit Points 250
Weight , kg 3834.0
Firepower 83
12.7 mm AN/M2 (W) 4
12.7 mm MG-53-2 (W) 4
Maneuverability 280
Average Time to Turn 360 deg , s 22.80
Rate of Roll , °/s 125
Controllability 94
Airspeed 545
Top Speed at Sea Level , km/h 480
Top Speed at Best Altitude , km/h 600
Maximum Dive Speed , km/h 800
Stall Speed , km/h 160
Rate of Climb , m/s 15.80
Optimum Airspeed , km/h 385
Altitude Performance , m 1850
Optimum Altitude , m 1850
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