Ikarus IK-1 Kracuj Corps Reconnaissance Aircraft
Powerplant: One BMW 132A nine-cylinder radial air cooled engine rated at 720hp (541kW)
Wing span: 13.94 m
Length: 10.54 m
Height: 3.25 m
Wing area: 30.844 sq. m
Empty weight: 2,166 kg
Loaded weight: 3,011 kg
Wing loading: 97.3 kg/sq. m
Power loading 4.2 kg/hp
Maximum speed: 322 km/hr at 1,220 m
Cruising speed: 275 km/hr
Rate of climb: 541 m/minute
Service ceiling: 7,360 m
Range: 700 km
Layout comprises pilot and observer in tandem under glazed canopy. One fixed 7.92mm M33 machinegun with 500 rounds in front fuselage decking, synchronised to fire through the propeller arc; one flexible 7.92mm M33 machinegun with 1,000 rounds in rear cockpit.
Radio equipment fitted in observer’s cockpit with windmill generator and fixed as well as trailing antennas. A topographical camera is normally fitted behind the observer and there is stowage for a hand camera in the observer’s cockpit. The fixed camera can be replaced by two bomb containers each carrying five 10kg. bombs; provision for installation of smoke screen apparatus in place of cameras or bomb containers.