Aero A.46: Difference between revisions
Content deleted Content added
add specifications template |
Removing Commons category link that doesn't match this article |
||
| (26 intermediate revisions by 20 users not shown) | |||
| Line 1: | Line 1: | ||
{{Unreferenced|date=December 2009}} |
|||
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. |
|||
{|{{Infobox aircraft begin |
|||
|name = A.46<!-- avoid stating manufacturer (it's stated 3 lines below) unless name used by other aircraft manufacturers --> |
|||
|image = <!--in the ''Image:filename'' format with no image tags--> |
|||
|caption = <!--Image caption; if it isn't descriptive, please skip--> |
|||
}} |
|||
{{Infobox aircraft type |
|||
|type = Trainer |
|||
|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:. --> |
|||
|manufacturer = Aero |
|||
|designer = <!--Only appropriate for single designers, not project leaders--> |
|||
|first flight = <!--If this hasn't happened, skip this field!--> |
|||
|introduced = <!--Date the aircraft entered or will enter military or revenue service--> |
|||
|retired = <!--Date the aircraft left service. If vague or more than a few dates, skip this --> |
|||
|status = <!--In most cases, redundant; use sparingly--> |
|||
|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. --> |
|||
|more users = <!-- Limited to THREE (3) 'more users' here (4 total users). Separate users with <br/>. --> |
|||
|produced = <!--Years in production (eg. 1970-1999) if still in active use but no longer built --> |
|||
|number built = 1 |
|||
|program cost = <!--Total program cost--> |
|||
|unit cost = <!--Incremental or flyaway cost for military or retail price for commercial aircraft--> |
|||
|developed from = <!--The aircraft which formed the basis for this aircraft--> |
|||
|variants with their own articles = <!--Variants OF this aircraft--> |
|||
}} |
|||
|} |
|||
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]]. |
|||
==Specifications (A.46)== |
==Specifications (A.46)== |
||
{{ |
{{Aircraft specs |
||
{{aircraft specifications |
|||
|plane or copter?=plane |
|||
|jet or prop?=prop |
|||
|ref= |
|ref= |
||
|prime units?=met |
|||
<!-- |
|||
General characteristics |
|||
--> |
|||
|crew=two, student and instructor |
|crew=two, student and instructor |
||
|length m=8.45 |
|||
|capacity= |
|||
|span m=11.82 |
|||
|payload main= |
|||
|wing area sqm=32.6 |
|||
|payload alt= |
|||
|empty weight kg=1,134 |
|||
|length main= 8.45 m |
|||
|gross weight kg=1,488 |
|||
|length alt= 27 ft 9 in |
|||
<!-- |
|||
|span main= 11.82 m |
|||
Powerplant |
|||
|span alt= 38 ft 9 in |
|||
--> |
|||
|height main= |
|||
|eng1 number=1 |
|||
|height alt= |
|||
|eng1 name=Skoda-built [[Hispano-Suiza 8Fb]] |
|||
|area main= 32.6 m² |
|||
|eng1 type=V-8 water-cooled piston engine |
|||
|area alt= 351 ft² |
|||
|eng1 kw=224<!-- prop engines --> |
|||
|airfoil= |
|||
<!-- |
|||
|empty weight main= 1,134 kg |
|||
Performance |
|||
|empty weight alt= 2,495 lb |
|||
--> |
|||
|loaded weight main= 1,488 kg |
|||
|max speed kmh=196 |
|||
|loaded weight alt= 3,274 lb |
|||
|ceiling m=4,850 |
|||
|useful load main= |
|||
|climb rate ms=2.783 |
|||
|useful load alt= |
|||
|wing loading kg/m2=46 |
|||
|max takeoff weight main= |
|||
|power/mass=0.150 W/kg (0.09 hp/lb) |
|||
|max takeoff weight alt= |
|||
|more general= |
|||
|engine (prop)= Skoda-built [[Hispano-Suiza 8]]Fb |
|||
|type of prop= |
|||
|number of props=1 |
|||
|power main= 224 kW |
|||
|power alt= 300 hp |
|||
|power original= |
|||
|max speed main=196 km/h |
|||
|max speed alt= 123 mph |
|||
|cruise speed main= |
|||
|cruise speed alt= |
|||
|stall speed main= |
|||
|stall speed alt= |
|||
|never exceed speed main= |
|||
|never exceed speed alt= |
|||
|range main= |
|||
|range alt= |
|||
|ceiling main= 4,850 m |
|||
|ceiling alt= 15,908 ft |
|||
|climb rate main= 167 m/min |
|||
|climb rate alt= 547 ft/min |
|||
|loading main= 46 kg/m² |
|||
|loading alt=9.3 lb/ft² |
|||
|thrust/weight= |
|thrust/weight= |
||
|power/mass main=150 W/kg |
|||
|power/mass alt=0.09 hp/lb |
|||
|more performance= |
|||
|armament= |
|||
|avionics= |
|||
}} |
}} |
||
== |
==See also== |
||
{{ |
{{Aircontent| |
||
|related= |
|related= |
||
|similar aircraft= |
|similar aircraft= |
||
|sequence= |
|||
[[Aero A.35|A.35]] - |
|||
[[Aero A.38|A.38]] - |
|||
[[Aero A.42|A.42]] - |
|||
'''A.46''' - |
|||
[[Aero A.100|A.100]] - |
|||
[[Aero A.101|A.101]] - |
|||
[[Aero A.102|A.102]] |
|||
|lists= |
|lists= |
||
|see also= |
|see also= |
||
}} |
}} |
||
{{Aero Vodochody aircraft}} |
|||
[[Category:Czechoslovakian military trainer aircraft 1930-1939]] |
|||
[[Category:1930s Czechoslovakian military trainer aircraft]] |
|||
{{aero-1930s-stub}} |
|||
[[Category:Aero Vodochody aircraft|A046]] |
|||
[[Category:Biplanes]] |
|||
[[Category:Single-engined tractor aircraft]] |
|||
Latest revision as of 18:27, 17 April 2020
 |
| 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]