Ikarus Aero 2

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Aero 2
Type	Trainer
Manufacturer	Ikarus
Maiden flight	1940
Introduced	1948
Retired	1959
Primary user	Yugoslav Air Force
Number built	248

The Ikarus Aero 2 was a piston-engined military trainer aircraft built in Yugoslavia in the years following World War II, although the design pre-dated the war.

Contents 1 Development 2 Description 3 Variants 4 Operators 5 Specifications 5.1 General characteristics 5.2 Performance 6 Related content 7 References 8 External links

[edit] Development

It was designed in response to a Yugoslav Air Force requirement for a modern, monoplane trainer to replace the Fizir FN biplanes then in service. The powerplant was to be the de Havilland Gipsy Major because of its successful use in similar trainer aircraft built in other countries.

Ikarus' entry, designed by Boris Cijan and Djordje Petkovic was selected over its two competitors in trials held between June and November 1940, but production did not take place until the Air Force began to rebuild itself after the war. 248 were eventually built, serving from 1948 to 1959 (380 built according to ^[1].

[edit] Description

The Aero 2 was a low wing design that seated the student and instructor in tandem, open cockpits (although later versions added a canopy to enclose them). Undercarriage was fixed and used a tailskid.

[edit] Variants

• Aero 2B : Open cockpit version.
• Aero 2BE : Enclosed cockpit version.
• Aero 2C : Open cockpit version.
• Aero 2D : Enclosed cockpit version.
• Aero 2E : Enclosed cockpt version.
• Aero 2F : Open cockpit version.
• Aero 2H : Two-seat floatplane version.

[edit] Operators

•  Yugoslavia
  • SFR Yugoslav Air Force

[edit] Specifications

[edit] General characteristics

• Crew: two, student and instructor
• Length: 8.23 m (27 ft 0 in)
• Wingspan: 10.50 m (30 ft 5 in)
• Height: 2.64 m (8 ft 8 in)
• Wing area: 17.4 m² (187 ft²)
• Empty: 564 kg (1,241 lb)
• Loaded: kg ( lb)
• Maximum takeoff: 978 kg (2,152 lb)
• Powerplant: 1x de Havilland Gipsy Major 10, 108 kW (145 hp)

[edit] Performance

• Maximum speed: 224 km/h (140 mph)
• Range: 745 km (466 miles)
• Service ceiling: 4,930 m (16,170 ft)
• Rate of climb: m/min ( ft/min)
• Wing loading: kg/m² ( lb/ft²)
• Power/Mass: kW/kg ( hp/lb)

[edit] Related content

Related development:

Comparable aircraft:

• Miles Magister - RWD-23

Designation sequence: Aero 2 - Aero 3

[edit] References

[edit] External links

• Photos and drawings at Ugolok Neba

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