Aero A.25: Difference between revisions
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* '''Empty:''' 985 kg (2,167 lb) |
* '''Empty:''' 985 kg (2,167 lb) |
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* '''Loaded:''' 1,270 kg (2,794 lb) |
* '''Loaded:''' 1,270 kg (2,794 lb) |
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* '''Maximum takeoff:''' kg ( lb) |
* '''Maximum takeoff:''' kg ( lb) |
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* '''Powerplant:''' 1x [[BMW III]]a, 138 kW (185 hp) |
* '''Powerplant:''' 1x [[BMW III]]a, 138 kW (185 hp) |
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===Performance=== |
===Performance=== |
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* '''Maximum speed:''' 160 km/h (100 mph) |
* '''Maximum speed:''' 160 km/h (100 mph) |
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* '''Range:''' km ( miles) |
* '''Range:''' km ( miles) |
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* '''Service ceiling:''' 6,500 m (21,320 ft) |
* '''Service ceiling:''' 6,500 m (21,320 ft) |
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* '''Rate of climb:''' 240 m/min (787 ft/min) |
* '''Rate of climb:''' 240 m/min (787 ft/min) |
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* '''Wing loading:''' 35 kg/m² (7.1 lb/ft²) |
* '''Wing loading:''' 35 kg/m² (7.1 lb/ft²) |
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* '''Power/ |
* '''Power/mass:''' 110 W/kg (0.07 hp/lb) |
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==Related content== |
==Related content== |
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Revision as of 19:37, 7 September 2005
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 (A.25)
General characteristics
- Crew: two, student and instructor
- Length: 8.10 m (26 ft 8 in)
- Wingspan: 12.80 m (43 ft 0 in)
- Height: 3.10 m (10 ft 2 in)
- Wing area: 36.2 m² (389 ft²)
- Empty: 985 kg (2,167 lb)
- Loaded: 1,270 kg (2,794 lb)
- Powerplant: 1x BMW IIIa, 138 kW (185 hp)
Performance
- Maximum speed: 160 km/h (100 mph)
- Service ceiling: 6,500 m (21,320 ft)
- Rate of climb: 240 m/min (787 ft/min)
- Wing loading: 35 kg/m² (7.1 lb/ft²)
- Power/mass: 110 W/kg (0.07 hp/lb)
Related content
Related development: A.11 - A.12 - A.21 - A.22 - A.29
Comparable aircraft:
Designation sequence: A.22 - A.23 - A.24 - A.25 - A.26 - A.27 - A.29