An attempt to adapt the serial Tu-2 for jet engines. The aircraft was tested in 1947-1948. A small series of planes were built, they were used as testbed aircraft and for crew training.
-
3,600,000
Price
-
126,000
Research price
Restore standard configuration
Engine
21600
RD-45F
26400
VK-1
Cowling-mounted weapon
24000
23 mm NR-23 (C)
Top turret
24000
B-20ENT
Bottom turret
24000
B-20ENT
Premium aircraft
Special aircraft
|
Gun Armament
|
14
|
| 23 mm NS (C) |
1
|
| 23 mm NR-23 (C) |
1
|
| Turret 12.7 mm UBT |
1
|
| Turret B-20ENT |
1
|
| Turret 12.7 mm UBT |
1
|
| Turret B-20ENT |
1
|
|
Bombs and Rockets
|
46
|
| FAB-500 |
4
|
|
Survivability
|
58
|
|
Hit Points
|
1800
|
|
Airspeed
|
64
|
|
Top Speed at Best Altitude,
|
770
|
|
Maximum Dive Speed,
|
880
|
|
Maneuverability
|
18
|
|
Average Time to Turn 360 deg,
|
19.60
|
|
Rate of Roll,
|
55
|
|
Optimum Airspeed,
|
513
|
|
Stall Speed,
|
160
|
|
Altitude Performance
|
86
|
|
Optimum Altitude,
|
2600
|
|
Rate of Climb,
|
105.50
|
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.
