Curtiss P-23 Fighter II tier 1
Pilot

Experimental all-metal fighter aircraft developed on the basis of the successful P-6E with several prototypes being produced.

Effective in mid-altitude combat
Excellent horizontal maneuverability
  • 3,300
    Price
  • 130
    Research price

Configuration Curtiss P-23

Engine
I
0
Engine V-1570-1
Specifications:
Engine Type water-cooled
Weight , kg 320.0
Power 600
Compatibility: Curtiss P-23
I
V-1570-1
II
185
Engine V-1570-23
Specifications:
Engine Type water-cooled
Weight , kg 340.0
Power 650
Price:
Research price 185
Purchase price 1,610
Compatibility: Curtiss P-23
II
185
V-1570-23
III
220
Engine V-1570-59
Specifications:
Engine Type water-cooled
Weight , kg 350.0
Power 675
Price:
Research price 220
Purchase price 2,470
Compatibility: Curtiss P-23
III
220
V-1570-59
Airframe
I
0
Airframe XP-23
Specifications:
Weight , kg 1360.0
Hit Points 65
Compatibility: Curtiss P-23
I
XP-23
II
160
Airframe P-23
Specifications:
Weight , kg 1400.0
Hit Points 85
Price:
Research price 160
Purchase price 3,200
Compatibility: Curtiss P-23
II
160
P-23
Synchronized machine gun
I
0
MACHINEGUN_SMALL_LOW_DESCRIPTION 7.62 mm M1919A4 (S)
Sustained fire without overheating
Effective against maneuvering targets
Specifications:
Damage per Second 17
Rate of Fire , rounds/min 600
Effective Fire Range , m 380
I
7.62 mm M1919A4 (S)
Synchronized machine gun
I
0
MACHINEGUN_SMALL_LOW_DESCRIPTION 7.62 mm M1919A4 (S)
Sustained fire without overheating
Effective against maneuvering targets
Specifications:
Damage per Second 17
Rate of Fire , rounds/min 600
Effective Fire Range , m 380
I
7.62 mm M1919A4 (S)
III
360
Machine gun 12.7 mm BMG1921 (S)
Sustained fire without overheating
Effective against maneuvering targets
Specifications:
Damage per Second 28
Rate of Fire , rounds/min 500
Effective Fire Range , m 440
Price:
Research price 360
Purchase price 7,800
III
360
12.7 mm BMG1921 (S)

Specifications

Hit Points 65
Weight , kg 1740.0
Firepower 18
7.62 mm M1919A4 (S) 1
7.62 mm M1919A4 (S) 1
12.7 mm BMG1921 (S) 1
Maneuverability 397
Average Time to Turn 360 deg , s 9.00
Rate of Roll , °/s 100
Controllability 94
Airspeed 319
Top Speed at Sea Level , km/h 315
Top Speed at Best Altitude , km/h 350
Maximum Dive Speed , km/h 480
Stall Speed , km/h 70
Rate of Climb , m/s 9.10
Optimum Airspeed , km/h 218
Altitude Performance , m 900
Optimum Altitude , m 900
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