Aero Ae 01: Difference between revisions
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==Specifications (Ae 01)== |
==Specifications (Ae 01)== |
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{{Aircraft |
{{Aircraft specs |
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|plane or copter?=plane |
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|jet or prop?=prop |
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|ref= |
|ref= |
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|prime units?=met |
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|crew=two, student and instructor |
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|capacity= |
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General characteristics |
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|payload main= |
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--> |
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|payload alt= |
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|crew=2 |
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|length main= 8.50 m |
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|length |
|length m=8.5 |
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|span |
|span m=12.3 |
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|wing area sqm=35 |
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|span alt= 40 ft 4 in |
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|height main= |
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|height alt= |
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|area main= 35 m² |
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Powerplant |
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|area alt= 377 ft² |
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--> |
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|airfoil= |
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|eng1 number=1 |
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|eng1 name=[[Mercedes D.I]] |
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|empty weight alt= 1,573 lb |
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|eng1 type=6-cyl. water-cooled in-line piston engine |
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|loaded weight main= |
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|eng1 hp=100<!-- prop engines --> |
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| ⚫ | |||
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|useful load main= |
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Performance |
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|useful load alt= |
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|max takeoff weight main= 933 kg |
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|max |
|max speed kmh=110 |
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|more general= |
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|engine (prop)= Mercedes inline |
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|type of prop= |
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|number of props=1 |
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|power main= |
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|power alt= |
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|power original= |
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|max speed main=110 km/h |
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|max speed alt= 69 mph |
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|cruise speed main= |
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|cruise speed alt= |
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|stall speed main= |
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|stall speed alt= |
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|never exceed speed main= |
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|never exceed speed alt= |
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|range main= |
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|range alt= |
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|ceiling main= |
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|ceiling alt= |
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|climb rate alt= 345 ft/min |
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|loading main= |
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|loading alt= |
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|thrust/weight= |
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|power/mass main= |
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|power/mass alt= |
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|more performance= |
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|armament= |
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|avionics= |
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}} |
}} |
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{{Aero specs missing}} |
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==Operators== |
==Operators== |
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Revision as of 01:16, 20 March 2012
| Ae 01 | |
|---|---|
| |
| Role | Trainer |
| National origin | Czechoslovakia |
| Manufacturer | Aero |
| First flight | 1919 |
| Developed from | Hansa-Brandenburg B.I |
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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.
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 Ae 10 - Aero A.14
 | This article on an aircraft of the 1920s is a stub. You can help Wikipedia by expanding it. |