Jump to content

Aero Ae 01: Difference between revisions

From Wikipedia, the free encyclopedia
Content deleted Content added
No edit summary
KaRei (talk | contribs)
Added earlier designation Ae 10 and army designation A-1.
Line 26: Line 26:
|}
|}


The '''[[Aero Vodochody|Aero]] Ae 01''' was a [[Czechoslovakia]]n military [[trainer aircraft|trainer]] [[biplane]] built in [[1919 in aviation|1919]], the company's first attempt to modify one of the aircraft designs they had been manufacturing under licence during [[World War I]], the [[Hansa-Brandenburg B.I]].
The '''[[Aero Vodochody|Aero]] Ae 01''' was a [[Czechoslovakia]]n military [[trainer aircraft|trainer]] [[biplane]] built in [[1919 in aviation|1919]], the company's first attempt to modify one of the aircraft designs they had been manufacturing under licence during [[World War I]], the [[Hansa-Brandenburg B.I]]. The project was originally designated as Ae 10, but later re-designated to Ae 01. The army operated the aircraft under designation A-1.


==Specifications (Ae 01)==
==Specifications (Ae 01)==
Line 63: Line 63:
|related=
|related=
[[Hansa-Brandenburg B.I]] -
[[Hansa-Brandenburg B.I]] -
[[Aero Ae 10]] -
[[Aero A.14]]
[[Aero A.14]]
|similar aircraft=
|similar aircraft=

Revision as of 06:20, 21 April 2017

Ae 01
Role Trainer
National origin Czechoslovakia
Manufacturer Aero
First flight 1919
Developed from Hansa-Brandenburg B.I

The Aero Ae 01 was a Czechoslovakian military trainer biplane built in 1919, the company's first attempt to modify one of the aircraft designs they had been manufacturing under licence during World War I, the Hansa-Brandenburg B.I. The project was originally designated as Ae 10, but later re-designated to Ae 01. The army operated the aircraft under designation A-1.

Specifications (Ae 01)

General characteristics

  • Crew: 2
  • Length: 8.5 m (27 ft 11 in)
  • Wingspan: 12.3 m (40 ft 4 in)
  • Wing area: 35 m2 (380 sq ft)
  • Empty weight: 715 kg (1,576 lb)
  • Gross weight: 933 kg (2,057 lb)
  • Powerplant: 1 × Mercedes D.I 6-cyl. water-cooled in-line piston engine, 75 kW (100 hp)

Performance

  • Maximum speed: 110 km/h (68 mph, 59 kn)
  • Rate of climb: 1.75 m/s (344 ft/min)

Operators

See also

Related development Hansa-Brandenburg B.I - Aero A.14

References