Aero Ae 04

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The Aero Ae 04 was a Czechoslovakian biplane fighter aircraft of 1921. A development of the Ae 02, it was no more successful than its predecessor in attracting purchase orders, and it flew only in prototype form. Undaunted by the lack of interest, development continued as the A.18.

Contents

[edit] Specifications (Ae 04)

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[edit] General characteristics

  • Crew: one, pilot
  • Length: 5.60 m (18 ft 4 in)
  • Wingspan: 7.70 m (25 ft 3 in)
  • Height: 2.70 m (8 ft 10 in)
  • Wing area: 14.6 m² (157 ft²)
  • Empty: 670 kg (1,474 lb)
  • Loaded: kg ( lb)
  • Maximum takeoff: 900 kg (1,980 lb)
  • Powerplant: 1x BMW IIIa, 138 kW (185 hp)

[edit] Performance

  • Maximum speed: 225 km/h (69 mph)
  • Range: km ( miles)
  • Service ceiling: 6,362 m (20,876 ft)
  • Rate of climb: 357 m/min (1,171 ft/min)
  • Wing loading: kg/m² ( lb/ft²)
  • Power/mass: W/kg ( hp/lb)

[edit] Armament

[edit] Related content

Related development: Aero Ae 02 - Aero A.18

Comparable aircraft:

Designation sequence: Ae 01 - Ae 02 - Ae 03 - Ae 04 - Ae 10

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