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Aero A.102

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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.

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


See also

Comparable aircraft

Related lists

Template:Aero Vodochody aircraft


cs:Aero A-102 de:Aero A.102 fr:Aero A.102 nl:Aero A-102

This article is licensed under the GNU Free Documentation License.
It uses material from the Wikipedia article "Aero A.102".