Aero A.102

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Aero A.102
Type Fighter aircraft
Manufacturer Aero Vodochody
Maiden flight 1934
Introduced n/a
Primary user Czech Air Force

The Aero A.102 was a Czechoslovakian fighter aircraft that flew in prototype form in 1934. It was developed in response to a Czech Air Force requirement of that year, but was passed over in favour of the Avia B.35.

The A.102 was of gull winged monoplane configuration with tailwheel undercarriage, and was perhaps inspired by the successful PZL P.11.

[edit] Specifications (A.102)

General characteristics

  • Crew: 1
  • Length: 7.30 m (23 ft 11 in)
  • Wingspan: 11.50 m (37 ft 9 in)
  • Height: m (ft in)
  • Wing area: 18.50 m² (199 ft²)
  • Empty weight: 1,478 kg (3,252 lb)
  • Loaded weight: 2,036 kg (4,479 lb)
  • Max takeoff weight: kg (lb)
  • Powerplant: 1× Walter-built Gnome-Rhône Mistral Major 14Kfs, 900 hp (670 kW)

Performance

Armament

[edit] Related content

 

Comparable aircraft

Designation sequence

Related lists

 

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