I-153
Technical details
Constructed by: Nikolai N Polikarpov.
Type: Single-seat fighter (15bis and 153 fighter-bomber).
Powerplant: (I-15) one 700 hp Svetsov M-25 (Wright "Cyclone"), (I-15bis) 750 hp M-25B, (I-153) 1 000 hp M-63, all nine-cylinder radial piston engines.
Dimensions: Span 9,13 m, (I-15bis) 10,21 m, (I-153) 10 m; length 6,29 m, (I-15bis) 6,33 m, (I-153) 6,17 m; height 2,92 m, (I-15bis) 3,0 m, (I-153) 2,82 m.
Weights: Empty 1 180 kg, (I-15bis) 1 305 kg, (I-153) 1 440 kg; maximum loaded 1 370-1 422 kg, (I-15bis) 1 900 kg, (I-153) 2 010 kg.
Performance: Maximum speed 360 km/h, (I-15bis) 370 km/h, (I-153) 430 km/h;
rate of climb some 765 m/min;
service ceiling 10 000 m, (I-15bis) 8 000 m, (I-153) 10 700 m;
range 720 km, (I-15bis) 450 km, (I-153) 480 km.
Armament: (I-15) four (sometimes two) 7,62 mm DA or SjKAS machine-guns in the fuselage; (I-15bis) same as the I-15 plus two 50 kg bombs or six RS-82 rocket projectiles; (I-153) same as the I-15 but with 75 kg bombs.
History: First flight (TsKB) October 1933, entered service in 1934, (I-15bis) entered service in 1937, (I-153) entered service in 1939.
Used by: Finland (captured Soviet aircraft), China, Soviet Union, Spain (both sides).
I-16
Technical details
Specifications (I-16 Type 24):
Engine: One 1,000-hp M-62 radial piston engine
Weight: Empty 1,475. kilos.,
Max Takeoff 2,060. kilos.
Wing Span: 8.9 ms.
Length: 6.088 ms.
Height: 2.17 ms.
Performance:
Maximum Speed at 3,048 ms: 490 Kph
Ceiling: 9,470 ms
Range: 600 kilometres
Armament:
Four 7.62-mm (0.3-inch) Sh KAS machine guns (Two in forward fuselage; two in wings)
Up to 200 kilos of bombs or six RS-82 rockets on underwing racks
Although the I-16 was faster, it was both less manouevrable and more unstable in flight. The I-153 seems to have carried the heavier armament so all things being equal perhaps the I-153 would have come out on top.
my 0.23c
Kiwimac