Aero A.46: Difference between revisions
Content deleted Content added
No edit summary |
No edit summary |
||
| Line 1: | Line 1: | ||
The '''[[Aero Vodochody|Aero]] A.46''' was a [[Czechoslovakia]]n [[ |
The '''[[Aero Vodochody|Aero]] A.46''' was a [[Czechoslovakia]]n military [[trainer aircraft|trainer]] [[biplane]] that flew in prototype form in [[1931 in aviation|1931]]. No mass production resulted. |
||
==Specifications (A.46)== |
==Specifications (A.46)== |
||
Revision as of 02:21, 16 September 2004
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: 0.15 kW/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