Aero A.46: Difference between revisions
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Revision as of 22:23, 28 July 2019
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| A.46 | |
|---|---|
| Role | Trainer |
| National origin | Czechoslovakia |
| Manufacturer | Aero |
| Number built | 1 |
The Aero A.46 was a Czechoslovakian military trainer biplane that flew in prototype form in 1931. No mass production resulted from Aero.
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)
- Wing area: 32.6 m2 (351 sq ft)
- Empty weight: 1,134 kg (2,500 lb)
- Gross weight: 1,488 kg (3,280 lb)
- Powerplant: 1 × Skoda-built Hispano-Suiza 8Fb V-8 water-cooled piston engine, 224 kW (300 hp)
Performance
- Maximum speed: 196 km/h (122 mph, 106 kn)
- Service ceiling: 4,850 m (15,910 ft)
- Rate of climb: 2.783 m/s (547.8 ft/min)
- Wing loading: 46 kg/m2 (9.4 lb/sq ft)
- Power/mass: 0.150 W/kg (0.09 hp/lb)
See also
Media related to Aero A.46 at Wikimedia Commons