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» Economics » Aero » Topics begins with A » Aero Ae-45

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The aero Ae-45 was a twin-engine passenger aircraft of the Czechoslovakian manufacturer aero with seat in Prague Vysocani. Militarily it was used as liaison aircraft.

The development began 1946 and by the technical designers Jiri Bouzek, Ondrej Nemec and Franti"šek Vik were accomplished. The prototype (identification: OK-BCA) flew for the first time on 21 July 1947, the second with the identification OK-CDA one year later. Flight testing ran without incidents and the machine for series production was released and until 1951 in 200 copies built, which except in the CSSR still in Italy, Hungary, which USSR and Switzerland flew. The Ae-45 was used also briefly at Czechoslovakian air forces, it carried there the designation K-75

1954 appeared the improved execution Ae-45S super aero, their production of the company Let in Uh. - Hradi"šte Kunovice was taken over, since with aero at this time the series production of the MiG-15-Lizenz S-102 had priority. Developed again 228 machines, which were also exported. Some Ae-45S received radios and were night flight suited.

China acquired the license rights and built those for super aero under the name Suingari-1 under license. The interflight as well as air forces of the NVA had some copies of this type likewise in their existence.

1959 appeared the Ae-145 as advancement with stronger M 332 engines, by which 162 pieces with Let were produced. The successors Ae-245 and Ae-345 remained experimental models.

Technical description: The Ae-45 was a cantilever low-wing aircraft in complete metal semi-monocoque structure. The wing was three-part with 3 cross-beams, the tail unit was cantilever in normal building method. All rudders were material-covered. The main wheels of the tail wheel chassis brought backwards into the engine cars, the tail landing gear in were rigid. In the winter landing skis could be installed.

Technical data (aero Ae-45S)

  • Span: 12.25 m
  • Length: 7.54 m
  • Height: 2.35 m
  • Wing area: 17.09 m
  • Empty weight: 960 kg
  • Takeoff weight: 1,600 kg
  • Drive: two air-cooled 4-Zylinder-Reihenmotoren walter Minor 4-III with ever 77 KW of take-off power
  • Maximum speed: 265 km/h
  • Cruising speed: 230 km/h
  • Rate of climb: 5 m/s
  • Ceiling: 4,350 kg
  • Range: 1,350 km
  • Crew/passengers: 1/3

See also: List of the types of aircraft

Articles in category "Aero Ae-45"

We found here 15 articles.


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