Aero A.25
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| 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)
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 qater-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
See also
Related lists
References
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.