Aero A.46: Difference between revisions
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* '''Wingspan:''' 11.82 m (38 ft 9 in) |
* '''Wingspan:''' 11.82 m (38 ft 9 in) |
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* '''Height:''' m ( ft in) |
* '''Height:''' m ( ft in) |
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* '''Wing area:''' 32.6 m |
* '''Wing area:''' 32.6 m² (351 ft²) |
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* '''Empty:''' 1,134 kg (2,495 lb) |
* '''Empty:''' 1,134 kg (2,495 lb) |
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* '''Loaded:''' 1,488 kg (3,274 lb) |
* '''Loaded:''' 1,488 kg (3,274 lb) |
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* '''Service ceiling:''' 4,850 m (15,908 ft) |
* '''Service ceiling:''' 4,850 m (15,908 ft) |
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* '''Rate of climb:''' 167 m/min (547 ft/min) |
* '''Rate of climb:''' 167 m/min (547 ft/min) |
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* '''Wing loading:''' 46 kg/m |
* '''Wing loading:''' 46 kg/m² (9.3 lb/ft²) |
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* '''Power/mass:''' 150 W/kg (0.09 hp/lb) |
* '''Power/mass:''' 150 W/kg (0.09 hp/lb) |
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Revision as of 19:20, 7 September 2005
The Aero A.46 was a Czechoslovakian military trainer biplane that flew in prototype form in 1931. No mass production resulted.
Specifications (A.46)
General characteristics
- Crew: two, student and instructor
- Length: 8.45 m (27 ft 9 in)
- Wingspan: 11.82 m (38 ft 9 in)
- Height: m ( ft in)
- Wing area: 32.6 m² (351 ft²)
- Empty: 1,134 kg (2,495 lb)
- Loaded: 1,488 kg (3,274 lb)
- Maximum takeoff: kg ( lb)
- Powerplant: 1x Skoda-built Hispano-Suiza 8Fb, 224 kW (300 hp)
Performance
- Maximum speed: 196 km/h (123 mph)
- Range: km ( miles)
- Service ceiling: 4,850 m (15,908 ft)
- Rate of climb: 167 m/min (547 ft/min)
- Wing loading: 46 kg/m² (9.3 lb/ft²)
- Power/mass: 150 W/kg (0.09 hp/lb)
Related content
Related development:
Comparable aircraft:
Designation sequence: A.35 - A.38 - A.42 - A.46 - A.100 - A.101 - A.102