Development started in 1946. The prototype first flew on September 5, 1947. The concept of the aircraft was constantly improved. The further development of the project resulted in the creation of the I-215.
-
3,520,000
Price
-
102,100
Research price
Restore standard configuration
Engine
23200
TR-1
31500
TR-1A
Cowling-mounted weapon
30400
3x37 mm N-37L (C)
36400
3x37 mm NN-37 (C)
Outboard weapon
1800
2xFAB-250
Premium aircraft
Special aircraft
|
Gun Armament
|
46
|
| 37 mm N-37 (C) |
3
|
| 37 mm N-37L (C) |
3
|
| 37 mm NN-37 (C) |
3
|
|
Bombs and Rockets
|
0
|
| FAB-250 |
2
|
|
Survivability
|
16
|
|
Hit Points
|
500
|
|
Airspeed
|
61
|
|
Top Speed at Best Altitude,
|
860
|
|
Maximum Dive Speed,
|
950
|
|
Maneuverability
|
49
|
|
Average Time to Turn 360 deg,
|
12.30
|
|
Rate of Roll,
|
100
|
|
Optimum Airspeed,
|
483
|
|
Stall Speed,
|
250
|
|
Altitude Performance
|
45
|
|
Optimum Altitude,
|
1500
|
|
Rate of Climb,
|
110.20
|
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.
