I-15bis

И-15бис

Family
I-15
Class
Fighter
Changes
Straight upper wing of larger span and area with the Clark YH section, new cowling and oil cooler, 1200 × 120 mm wheels, M-25V. Also known as I-152.
Produced
2,408
Crew
1
Length
6,275 mm
Wingspan
10,200 mm
Wing area
22.5 m²
Empty weight
1,310 kg
Normal takeoff weight
1,700 kg
Max takeoff weight
1,870 kg
Internal fuel
320 L
Engine
М-25В
Engines
1
Diameter
2,800 mm
Blades
2
Max speed
379 km/h
Max speed altitude
3,500 m
Service ceiling
9,800 m
Takeoff run
170 m
Landing speed
105 km/h
Turn time
10.5 s

Climb time

AltitudeTime, min
5,000 m6.8

Armament

WeaponCountRounds
PV-121,100
PV-12425

Service

≈ May 1939 – Sep 1939
13 Sep 1940 – 13 Sep 1940
≈ 22 Jun 1941 – Apr 1943