The BV P.212 was designed as part of the Luftwaffe's Emergency Fighter Program. Several concepts were developed. The BV P.212.03 version was selected as final. The first prototype was to make its first flight in the summer of 1945.
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3,550,000
Price
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140,000
Research price
Restore standard configuration
Engine
24600
Jumo 004 E
30800
HeS 011
Cowling-mounted weapon
3x30 mm MK-108 (1944) (C)
40900
3x20 mm MG-213/20 (C)
Outboard weapon
8500
4xWGr-210
22500
24xR4M
Premium aircraft
Special aircraft
|
Gun Armament
|
36
|
| 30 mm MK-108 (1944) (C) |
3
|
| 20 mm MG-213/20 (C) |
3
|
|
Bombs and Rockets
|
0
|
| WGr-210 |
4
|
| R4M |
24
|
|
Survivability
|
12
|
|
Hit Points
|
380
|
|
Airspeed
|
67
|
|
Top Speed at Best Altitude,
|
880
|
|
Maximum Dive Speed,
|
1040
|
|
Maneuverability
|
64
|
|
Average Time to Turn 360 deg,
|
10.80
|
|
Rate of Roll,
|
180
|
|
Optimum Airspeed,
|
504
|
|
Stall Speed,
|
220
|
|
Altitude Performance
|
64
|
|
Optimum Altitude,
|
2000
|
|
Rate of Climb,
|
148.00
|
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.
