Developed on request of the U.S. Army Air Corps after the production of the Р-43 Lancer and P-44 Rocket was discontinued. First flew in May 1941. A total of 171 P-47Bs were built and used for conducting flight trials and training of pilots.
-
905,000
Price
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28,000
Research price
Restore standard configuration
Engine
6400
R-2800-21
8600
R-2800-59
Airframe
10000
P-47D-22
Outboard weapon
2400
2x250 lb
3150
2x500 lb
Outboard weapon
1650
6x4.5'' M8
Premium aircraft
Special aircraft
This information will be updated
|
Gun Armament
|
18
|
| 12.7 mm AN/M2 (W) |
6
|
| 12.7 mm AN/M2 (W) |
8
|
|
Bombs and Rockets
|
0
|
| 250 lb |
2
|
| 500 lb |
2
|
| 4.5'' M8 |
6
|
|
Survivability
|
11
|
|
Hit Points
|
360
|
|
Airspeed
|
48
|
|
Top Speed at Best Altitude,
|
650
|
|
Maximum Dive Speed,
|
860
|
|
Maneuverability
|
43
|
|
Average Time to Turn 360 deg,
|
13.50
|
|
Rate of Roll,
|
140
|
|
Optimum Airspeed,
|
420
|
|
Stall Speed,
|
180
|
|
Altitude Performance
|
45
|
|
Optimum Altitude,
|
1500
|
|
Rate of Climb,
|
96.60
|
The specifications are shown for a crew with 100% proficiency.
Indicates the capacity to withstand enemy fire. Factors in aircraft durability and the coefficients of resistance to critical damage and fire.
Indicates the capacity to damage aerial targets with forward-firing autocannon and machine guns as well as defensive turrets. Factors in damage, range, and accuracy.
Indicates the capacity to damage ground targets with bombs and rockets. Factors in damage and resupply time.
Indicates the capacity to engage in maneuvering combat. Factors in time to turn 360 degrees and rate of roll.
Indicates the capacity to engage in combat at a high speed. Factors in airspeed, acceleration, and boost efficiency.
Indicates the capacity to engage in combat at a high altitude. Factors in the optimum altitude range and maximum flight altitude.
