Aero A.46: Difference between revisions
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{|{{Infobox aircraft begin |
{|{{Infobox aircraft begin |
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|name = A.46<!-- avoid stating manufacturer (it's stated 3 lines below) unless name used by other aircraft manufacturers --> |
|name = A.46<!-- avoid stating manufacturer (it's stated 3 lines below) unless name used by other aircraft manufacturers --> |
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The '''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 from [[Aero Vodochody|Aero]]. |
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{{Unreferenced|date=December 2009}} |
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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. |
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==Specifications (A.46)== |
==Specifications (A.46)== |
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{{ |
{{Aircraft specs |
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{{Aircraft specifications |
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|plane or copter?=plane |
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|jet or prop?=prop |
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|ref= |
|ref= |
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|prime units?=met |
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General characteristics |
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|crew=two, student and instructor |
|crew=two, student and instructor |
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|length m=8.45 |
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|capacity= |
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|span m=11.82 |
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|payload main= |
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|wing area sqm=32.6 |
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|payload alt= |
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|empty weight kg=1,134 |
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|length main= 8.45 m |
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|gross weight kg=1,488 |
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|length alt= 27 ft 9 in |
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|span main= 11.82 m |
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Powerplant |
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|span alt= 38 ft 9 in |
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|height main= |
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|eng1 number=1 |
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|height alt= |
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|eng1 name=Skoda-built [[Hispano-Suiza 8Fb]] |
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|area main= 32.6 m² |
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|eng1 type=V-8 water-cooled piston engine |
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|area alt= 351 ft² |
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|eng1 kw=224<!-- prop engines --> |
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|airfoil= |
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|empty weight main= 1,134 kg |
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Performance |
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|empty weight alt= 2,495 lb |
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|loaded weight main= 1,488 kg |
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|max speed kmh=196 |
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|loaded weight alt= 3,274 lb |
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|ceiling m=4,850 |
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|useful load main= |
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|climb rate ms=2.783 |
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|useful load alt= |
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|wing loading kg/m2=46 |
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|max takeoff weight main= |
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|power/mass=0.150 W/kg (0.09 hp/lb) |
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|max takeoff weight alt= |
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|more general= |
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|engine (prop)= Skoda-built [[Hispano-Suiza 8]]Fb |
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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= |
|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= |
|related= |
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|similar aircraft= |
|similar aircraft= |
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|sequence= |
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[[Aero A.35|A.35]] - |
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[[Aero A.38|A.38]] - |
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[[Aero A.42|A.42]] - |
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'''A.46''' - |
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[[Aero A.100|A.100]] - |
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[[Aero A.101|A.101]] - |
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[[Aero A.102|A.102]] |
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|lists= |
|lists= |
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|see also= |
|see also= |
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{{Aero Vodochody aircraft}} |
{{Aero Vodochody aircraft}} |
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{{Aviation lists}} |
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[[Category:Czechoslovakian military trainer aircraft 1930–1939]] |
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[[Category:Propeller aircraft]] |
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[[Category:Biplane aircraft]] |
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[[Category:Single-engine aircraft]] |
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{{Aero-1930s-stub}} |
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[[Category:1930s Czechoslovakian military trainer aircraft]] |
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[[fr:Aero A.46]] |
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[[ |
[[Category:Aero Vodochody aircraft|A046]] |
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[[Category:Biplanes]] |
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[[Category:Single-engined tractor aircraft]] |
Latest revision as of 18:27, 17 April 2020
A.46 | |
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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)[edit]
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[edit]