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Ikarus IK-2

Yugoslavia ·first flew 1935· fighter

what is it?

The Ikarus IK-2 was a 1930s high-wing, single-seat, monoplane fighter aircraft of Yugoslav design built for the Royal Yugoslav Army Air Force. The IK-2 was designed by French-trained engineers Kosta Sivčev and Ljubomir Ilić, who saw the desirability of developing a home-grown aircraft industry. A gull-wing design, it was armed with a hub-firing autocannon and fuselage-mounted synchronised machine guns.

How to recognise it: 1 piston engine with propeller · 11.4 m wingspan

base stats

  • speed 435 km/htop speed
  • range 700 kmwithout refuelling
  • size 1,857 kgmax take-off weight
  • built 14made in total

Bars compare against all aircraft: 3,500 km/h, 20,000 km, 850 seats; size and number built on a log scale up to 640 t (An-225) and 45,000 built (Cessna 172).

fun facts

  • First flew 91 years ago, in 1935.
  • Top speed is 3.3× a car on the Dutch motorway (130 km/h).
  • Wingspan of 11.4 m: about 3 cars parked nose to tail.
  • Can fly 1.4× higher than Mount Everest (8,849 m).

piston: A car-like piston engine turning a propeller: simple and cheap, the classic small plane.

spec sheet

first flight
1935-04-22
introduced
1935
retired
1945
status
retired
number built
14
role
fighter
origin
Yugoslavia
makers
Ikarbus
engines
1× Hispano-Suiza 12Ycrs
crew
1
length
7.9 m
wingspan
11.4 m
height
3.8 m
max take-off weight
1,857 kg
top speed
435 km/h
cruise speed
250 km/h
range
700 km
ceiling
12,000 m

Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.

Sources: Wikidata Q1658088, Wikipedia: Ikarus IK-2 (CC BY-SA 4.0).Updated 2026-10-24.

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