Aero A.25: Difference between revisions
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{{More citations needed|date=January 2021}} |
{{More citations needed|date=January 2021}} |
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{{Infobox aircraft |
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|name=Aero A.25 |
|name=Aero A.25 |
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|image= |
|image= |
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|caption= |
|caption= |
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}}{{Infobox aircraft type |
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|type=[[Trainer aircraft]] |
|type=[[Trainer aircraft]] |
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|manufacturer=[[Aero Vodochody]] |
|manufacturer=[[Aero Vodochody]] |
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|designer= |
|designer= |
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|first_flight=1920s |
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|introduction= |
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|introduced= |
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|retired= |
|retired= |
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|status= |
|status= |
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|primary_user=[[Czechoslovakia]] |
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|more_users= |
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|produced= |
|produced= |
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|number_built= |
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|number built= |
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|unit cost= |
|unit cost= |
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|variants |
|variants= |
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The '''Aero A.25''' was a [[biplane]] military [[trainer aircraft]] developed in [[Czechoslovakia]] from the [[Aero A.11]] reconnaissance-bomber and generally similar to the [[Aero A.21]] night trainer. |
The '''Aero A.25''' was a [[biplane]] military [[trainer aircraft]] developed in [[Czechoslovakia]] from the [[Aero A.11]] reconnaissance-bomber and generally similar to the [[Aero A.21]] night trainer. |
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|eng1 number=1 |
|eng1 number=1 |
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|eng1 name=[[BMW IIIa]] |
|eng1 name=[[BMW IIIa]] |
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|eng1 type=6-cylinder |
|eng1 type=6-cylinder water-cooled in-line piston engine |
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|eng1 kw=136 |
|eng1 kw=136 |
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==Operators== |
==Operators== |
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* [[Czechoslovakia]] |
* [[Czechoslovakia]] |
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==See also== |
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{{Aircontent |
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|related= |
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|similar aircraft= |
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|see also= |
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|lists= |
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* [[List of military trainer aircraft]] |
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}} |
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==References== |
==References== |
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Latest revision as of 22:33, 5 December 2024
 | This article needs additional citations for verification. (January 2021) |
| Aero A.25 | |
|---|---|
| General information | |
| Type | Trainer aircraft |
| Manufacturer | Aero Vodochody |
| Primary user | Czechoslovakia |
| History | |
| First flight | 1920s |
The Aero A.25 was a biplane military trainer aircraft developed in Czechoslovakia from the Aero A.11 reconnaissance-bomber and generally similar to the Aero A.21 night trainer.
Some A.25s were powered by the less powerful 134 kW (180 hp) Breitfeld & Danek Perun I engines, in which case they were designated Aero A.125.
Specifications (Aero A.25)
[edit]Data from Tschechoslowakische Flugzeuge : von 1918 bis heute[1]
General characteristics
- Crew: 2
- Length: 8.1 m (26 ft 7 in)
- Wingspan: 12.8 m (42 ft 0 in)
- Height: 3.1 m (10 ft 2 in) [citation needed]
- Wing area: 36.2 m2 (390 sq ft) [citation needed]
- Empty weight: 985 kg (2,172 lb) [citation needed]
- Gross weight: 1,270 kg (2,800 lb) [citation needed]
- Powerplant: 1 × BMW IIIa 6-cylinder water-cooled in-line piston engine, 136 kW (182 hp)
- Propellers: 2-bladed fixed-pitch propeller
Performance
- Maximum speed: 160 km/h (99 mph, 86 kn) [citation needed]
- Service ceiling: 6,500 m (21,300 ft) [citation needed]
- Rate of climb: 4 m/s (790 ft/min) [citation needed]
- Wing loading: 35 kg/m2 (7.2 lb/sq ft) [citation needed]
- Power/mass: 0.110 kW/kg (0.067 hp/lb)[citation needed]
Operators
[edit]References
[edit]
Wikimedia Commons has media related to Aero A.25.
- ^ Tschechoslowakische Flugzeuge : von 1918 bis heute (in German and English) (1st ed.). Berlin: Transpress : VEB verlag für Verkehrsween. 1987. p. 67. ISBN 3344001213.