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Aviation
␗I-153 M-62
I
Rank
AB
2.0
RB
2.3
SB
2.0
Battle rating
China
Research country
Fighter
Main role
4,000
RP
Research
2,100
SL
Purchase
China
Operator
General information

The I-153 M-62 "Chaika" was a Soviet single-engine piston fighter designed by the Polikarpov Design Bureau. It was an advancement of the I-15 and I-15bis models. Compared to its predecessors, the I-153 had improved aerodynamics. The characteristic gull-type upper wing was reinstated, and retractable landing gear was introduced. Additionally, the aircraft received a more powerful, higher-altitude M-62 engine with a variable-pitch propeller; its overall structure was reinforced; and an armored backplate was added to protect the pilot.

Despite its prolonged and problematic development process, the aircraft entered service in 1938 and saw action in several conflicts, including the Khalkhin Gol battles, the Soviet-Finnish War, and the early stages of the Great Patriotic War. It was also supplied abroad. From autumn 1937 to early 1941, 1,250 aircraft of various types were delivered to China. Of these, 93 were I-153 fighters received in the first half of 1940. That same year, three groups were formed from the delivered "Chaikas" and were used for air defense around major population centers. Most of these aircraft were lost in combat against Japanese fighters and bombers.

The Chinese I-153 M-62 was introduced in Update 1.91 "Night Vision". The "Chaika" stands out as an exceptional fighter in its class, offering outstanding turning performance, respectable speed, and a good climb rate for a biplane. It is also armed with four weak ShKAS machine guns, as well as able to carry unguided rockets or bombs. However, it has low structural durability, and its dive and level-flight speed are inferior to those of monoplanes.



Flight performance
Max speed
at 4,850 m 444410466425 km/h
Rate of Climb 15.211.420.111.4 m/s
Turn time 13.314.412.713.9 s
Max altitude 10,700 m
Takeoff Run 274 m

Landing
flaps
Take-off
flaps
Combat
flaps
Air
brake
General characteristics
Crew 1 person
Engine
Length 6.2 m
Wingspan 12.2 m
Wing Loading 83 kg/m²

Weight:
Base weight 1.61.651.561.64 t
Fuel in main tanks 0.24 t (1h 2m)

Limits:
Max Speed Limit (IAS) 580 km/h
Mach Number Limit 0.7 M
G limit ≈ -6/12 G
Gear Speed Limit (IAS) 450 km/h
Offensive armament
4 × 7.62 mm ShKAS machine gun
Ammunition 2,470 rounds
Fire rate 1,800 shots/min
One-second Burst Mass 0.29 kg

BeltBelt fillingArmor penetration (mm) at a distance:
10 m100 m500 m1000 m1500 m2000 m
T/Ball/Ball/AP-I/AI13127320
AP-I/AI/API-T13127320
AP-I/API-T13127320
AP-I/AP-I/AP-I/AI13127320
Suspended armament
Setup 1 2 × 50 kg FAB-50sv (forged) bomb
Setup 2 8 × ROS-82 rockets
Setup 3 8 × RBS-82 rockets
Economy
Repair cost Basic → Reference
AB 170 → 213 SL
RB 378 → 473 SL
SB 451 → 564 SL
Crew training 600 SL
Experts 2,100 SL
Aces 45 GE
Research Aces 110,000 RP
Reward multiplier AB / RB / SB
10 / 30 / 60 % SL
100 % RP
Total cost of modifications 4,420 RP
2,680 SL
Talisman cost 300 GE

Research order:
␗I-153 M-62

Flight performance
Survivability
Weaponry
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