Designed in 1946 under the influence of the German experience. The only prototype of the Su-9 was produced and tested in 1946–1947. The aircraft never entered service, since the project was abandoned in favor of the MiG-15.
-
2,400,000
Price
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82,500
Research price
Restore standard configuration
Engine
20400
RD-10A
23200
RD-10F
Cowling-mounted weapon
30400
2x23 mm NS-23KMU (C)
Outboard weapon
1800
2xFAB-250
Cowling-mounted weapon
18300
45 mm NS-45 (C)
Premium aircraft
Special aircraft
|
Gun Armament
|
30
|
| 23 mm NS-23KM (C) |
2
|
| 23 mm NS-23KMU (C) |
2
|
| 37 mm N-37 (C) |
1
|
| 45 mm NS-45 (C) |
1
|
|
Bombs and Rockets
|
0
|
| FAB-250 |
2
|
|
Survivability
|
14
|
|
Hit Points
|
450
|
|
Airspeed
|
54
|
|
Top Speed at Best Altitude,
|
810
|
|
Maximum Dive Speed,
|
900
|
|
Maneuverability
|
49
|
|
Average Time to Turn 360 deg,
|
12.30
|
|
Rate of Roll,
|
100
|
|
Optimum Airspeed,
|
409
|
|
Stall Speed,
|
200
|
|
Altitude Performance
|
42
|
|
Optimum Altitude,
|
1400
|
|
Rate of Climb,
|
107.80
|
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.
