Aero A.46: Difference between revisions
Content deleted Content added
replace depreceated infobox |
No edit summary |
||
| Line 29: | Line 29: | ||
==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 |
||
| ⚫ | |||
|capacity= |
|||
| ⚫ | |||
|payload main= |
|||
| ⚫ | |||
|payload alt= |
|||
| ⚫ | |||
| ⚫ | |||
| ⚫ | |||
|length alt= 27 ft 9 in |
|||
<!-- |
|||
| ⚫ | |||
Powerplant |
|||
|span alt= 38 ft 9 in |
|||
--> |
|||
|height main= |
|||
|eng1 number=1 |
|||
|height alt= |
|||
| ⚫ | |||
| ⚫ | |||
|eng1 type=V-8 water-cooled piston engine |
|||
|area alt= 351 ft² |
|||
|eng1 kw=224<!-- prop engines --> |
|||
|airfoil= |
|||
<!-- |
|||
| ⚫ | |||
Performance |
|||
|empty weight alt= 2,495 lb |
|||
--> |
|||
| ⚫ | |||
| ⚫ | |||
|loaded weight alt= 3,274 lb |
|||
| ⚫ | |||
|useful load main= |
|||
| ⚫ | |||
|useful load alt= |
|||
|wing loading kg/m2=46 |
|||
|max takeoff weight main= |
|||
| ⚫ | |||
|max takeoff weight alt= |
|||
|more general= |
|||
| ⚫ | |||
|type of prop= |
|||
|number of props=1 |
|||
|power main= 224 kW |
|||
|power alt= 300 hp |
|||
|power original= |
|||
| ⚫ | |||
|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 alt= 15,908 ft |
|||
|climb rate main= 167 m/min |
|||
| ⚫ | |||
|loading main= 46 kg/m² |
|||
|loading alt=9.3 lb/ft² |
|||
|thrust/weight= |
|thrust/weight= |
||
|power/mass main=150 W/kg |
|||
| ⚫ | |||
|more performance= |
|||
|armament= |
|||
|avionics= |
|||
}} |
}} |
||
Revision as of 15:41, 19 March 2012
| 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.
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)
- 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
 | This aircraft of the 1930s article is a stub. You can help Wikipedia by expanding it. |