Aero A.46: Difference between revisions
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==Specifications (A.46)== |
==Specifications (A.46)== |
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{{aero- |
{{aero-specs}} |
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{{aircraft specifications |
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===General characteristics=== |
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|plane or copter?=plane |
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|jet or prop?=prop |
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* '''Length:''' 8.45 m (27 ft 9 in) |
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|ref= |
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* '''Wingspan:''' 11.82 m (38 ft 9 in) |
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* '''Height:''' m ( ft in) |
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|capacity= |
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* '''Wing area:''' 32.6 m² (351 ft²) |
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|payload main= |
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* '''Empty:''' 1,134 kg (2,495 lb) |
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|payload alt= |
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* '''Loaded:''' 1,488 kg (3,274 lb) |
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|length main= 8.45 m |
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* '''Maximum takeoff:''' kg ( lb) |
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|length alt= 27 ft 9 in |
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|span main= 11.82 m |
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|span alt= 38 ft 9 in |
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===Performance=== |
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|height main= |
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* '''Maximum speed:''' 196 km/h (123 mph) |
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|height alt= |
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* '''Range:''' km ( miles) |
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|area main= 32.6 m² |
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* '''Service ceiling:''' 4,850 m (15,908 ft) |
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|area alt= 351 ft² |
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* '''Rate of climb:''' 167 m/min (547 ft/min) |
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|airfoil= |
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* '''Wing loading:''' 46 kg/m² (9.3 lb/ft²) |
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|empty weight main= 1,134 kg |
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* '''Power/mass:''' 150 W/kg (0.09 hp/lb) |
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|empty weight alt= 2,495 lb |
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|loaded weight main= 1,488 kg |
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|loaded weight alt= 3,274 lb |
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|useful load main= |
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|useful load alt= |
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|max takeoff weight main= |
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|max takeoff weight alt= |
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|more general= |
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|type of prop= |
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|number of props=1 |
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|power main= 224 kW |
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|power alt= 300 hp |
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|power original= |
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|max speed main=196 km/h |
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|max speed alt= 123 mph |
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|cruise speed main= |
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|cruise speed alt= |
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|stall speed main= |
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|stall speed alt= |
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|never exceed speed main= |
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|never exceed speed alt= |
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|range main= |
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|range alt= |
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|ceiling main= 4,850 m |
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|ceiling alt= 15,908 ft |
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|climb rate main= 167 m/min |
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|climb rate alt= 547 ft/min |
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|loading main= 46 kg/m² |
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|loading alt=9.3 lb/ft² |
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|thrust/weight= |
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|power/mass main=150 W/kg |
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|power/mass alt=0.09 hp/lb |
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|more performance= |
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|armament= |
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|avionics= |
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}} |
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==Related content== |
==Related content== |
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{{aircontent| |
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'''Related development:''' |
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|related= |
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|similar aircraft= |
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|sequence= |
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'''Designation sequence:''' |
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[[Aero A.35|A.35]] - |
[[Aero A.35|A.35]] - |
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[[Aero A.38|A.38]] - |
[[Aero A.38|A.38]] - |
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[[Aero A.102|A.102]] |
[[Aero A.102|A.102]] |
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|lists= |
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{{airlistbox}} |
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|see also= |
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}} |
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[[Category:Czechoslovakian military trainer aircraft 1930-1939]] |
[[Category:Czechoslovakian military trainer aircraft 1930-1939]] |
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{{aero-1930s-stub}} |
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Revision as of 10:53, 30 March 2007
The Aero A.46 was a Czechoslovakian military trainer biplane that flew in prototype form in 1931. No mass production resulted.
Specifications (A.46)
 |
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them. |
General characteristics
- Crew: two, student and instructor
Performance
Related content
| This aircraft of the 1930s article is a stub. You can help Wikipedia by expanding it. |