Aero A.46: Difference between revisions
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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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{|{{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 --> |
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|image = <!--in the ''Image:filename'' format with no image tags--> |
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|caption = <!--Image caption; if it isn't descriptive, please skip--> |
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}} |
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{{Infobox aircraft type |
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|type = Trainer |
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|national origin = [[Czechoslovakia]]<!-- Use the main nation (ie. UK), not constituent country (England); don't use "EU". List collaborative programs of only 2 or 3 nations; for more than 3, use "Multi-national:. --> |
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|manufacturer = Aero |
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|designer = <!--Only appropriate for single designers, not project leaders--> |
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|first flight = <!--If this hasn't happened, skip this field!--> |
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|introduced = <!--Date the aircraft entered or will enter military or revenue service--> |
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|retired = <!--Date the aircraft left service. If vague or more than a few dates, skip this --> |
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|status = <!--In most cases, redundant; use sparingly--> |
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|primary user = <!-- List only one user; for military aircraft, this is a nation or a service arm. Please DON'T add those tiny flags, as they limit horizontal space. --> |
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|more users = <!-- Limited to THREE (3) 'more users' here (4 total users). Separate users with <br/>. --> |
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|produced = <!--Years in production (eg. 1970-1999) if still in active use but no longer built --> |
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|number built = 1 |
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|program cost = <!--Total program cost--> |
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|unit cost = <!--Incremental or flyaway cost for military or retail price for commercial aircraft--> |
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|developed from = <!--The aircraft which formed the basis for this aircraft--> |
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|variants with their own articles = <!--Variants OF this aircraft--> |
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}} |
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|} |
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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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==Specifications (A.46)== |
==Specifications (A.46)== |
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{{Aircraft specs |
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{{aero-table}} |
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|ref= |
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===General characteristics=== |
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|prime units?=met |
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* '''Crew:''' two, student and instructor |
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* '''Length:''' 8.45 m (27 ft 9 in) |
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General characteristics |
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* '''Wingspan:''' 11.82 m (38 ft 9 in) |
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--> |
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* '''Height:''' m ( ft in) |
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|crew=two, student and instructor |
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* '''Wing area:''' 32.6 m² (351 ft²) |
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|length m=8.45 |
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* '''Empty:''' 1,134 kg (2,495 lb) |
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|span m=11.82 |
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* '''Loaded:''' 1,488 kg (3,274 lb) |
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|wing area sqm=32.6 |
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* '''Maximum takeoff:''' kg ( lb) |
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|empty weight kg=1,134 |
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* '''Powerplant:''' 1x Skoda-built [[Hispano-Suiza 8]]Fb, 224 kW (300 hp) |
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|gross weight kg=1,488 |
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===Performance=== |
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Powerplant |
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* '''Maximum speed:''' 196 km/h (123 mph) |
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--> |
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* '''Range:''' km ( miles) |
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|eng1 number=1 |
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* '''Service ceiling:''' 4,850 m (15,908 ft) |
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|eng1 name=Skoda-built [[Hispano-Suiza 8Fb]] |
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* '''Rate of climb:''' 167 m/min (547 ft/min) |
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|eng1 type=V-8 water-cooled piston engine |
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* '''Wing loading:''' 46 kg/m² (9.3 lb/ft²) |
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|eng1 kw=224<!-- prop engines --> |
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* '''Power/mass:''' 150 W/kg (0.09 hp/lb) |
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Performance |
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==Related content== |
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--> |
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'''Related development:''' |
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|max speed kmh=196 |
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|ceiling m=4,850 |
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'''Comparable aircraft:''' |
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|climb rate ms=2.783 |
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|wing loading kg/m2=46 |
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|power/mass=0.150 W/kg (0.09 hp/lb) |
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|thrust/weight= |
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}} |
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==See also== |
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'''Designation sequence:''' |
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{{Aircontent| |
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[[Aero A.35|A.35]] - |
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|related= |
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[[Aero A.38|A.38]] - |
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|similar aircraft= |
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[[Aero A.42|A.42]] - |
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|lists= |
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'''A.46''' - |
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|see also= |
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[[Aero A.100|A.100]] - |
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}} |
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[[Aero A.101|A.101]] - |
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[[Aero A.102|A.102]] |
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{{Aero Vodochody aircraft}} |
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{{airlistbox}} |
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[[Category:Czechoslovakian military trainer aircraft |
[[Category:1930s Czechoslovakian military trainer aircraft]] |
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[[Category:Aero Vodochody aircraft|A046]] |
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[[Category:Biplanes]] |
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[[Category:Single-engined tractor aircraft]] |
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Latest revision as of 18:27, 17 April 2020
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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)[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]