Aero A.104
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| Aero A.104 | |
|---|---|
| Type | Light bomber Reconnaissance aircraft |
| Manufacturer | Aero Vodochody |
| Maiden flight | 1937 |
| Status | Did not enter production |
| Number built | 2 |
The Aero A.104 was a biplane light bomber and reconnaissance aircraft built in Czechoslovakia during the 1930s. It was the final derivative of the A.100, and was essentially an Ab.101 with an enclosed cockpit. Although two different prototypes flew in 1937, it was not mass produced.
[edit] Specifications (A.104)
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: 2
- Length: 10.80 m (35 ft 5 in)
- Wingspan: 15.50 m (50 ft 10 in)
- Height: m (ft in)
- Wing area: 35.40 m² (380 ft²)
- Empty weight: kg (lb)
- Loaded weight: 3,100 kg (6,800 lb)
- Powerplant: 1× ČKD-built Hispano-Suiza 12Ydrs, 642 kW (860 hp)
Performance
- Maximum speed: 330 km/h (180 knots, 210 mph)
- Range: 1,000 km (540 nm, 630 mi)
- Service ceiling: 9,000 m (30,000 ft)
- Rate of climb: 6.8 m/s (1,340 ft/min)
- Wing loading: 88 kg/m² (18 lb/ft²)
- Power/mass: 0.21 W/kg (0.13 hp/lb)
Armament
- Bombs: 200 kg (440 lb)
[edit] Related content
Related development
Designation sequence
Related lists
- List of bomber aircraft
- List of military reconnaissance aircraft
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