Aero A.104
From Infogalactic: the planetary knowledge core
Lua error in package.lua at line 80: module 'strict' not found.
| A.104 | |
|---|---|
| Role | Light bomber Reconnaissance aircraft |
| Manufacturer | Aero Vodochody |
| First flight | 1937 |
| Status | Did not enter production |
| Number built | 2 |
The Aero A.104 was a parasol monoplane light bomber and reconnaissance aircraft built in Czechoslovakia during the 1930s. It was the final derivative of the Aero A.100, and was essentially an Aero Ab.101 with an enclosed cockpit and without the lower wing. Although two different prototypes flew in 1937, it was not mass-produced.
Specifications (A.104)
General characteristics
- Length: 10.8 m (35 ft 5 in)
- Wingspan: 15.5 m (50 ft 10 in)
- Wing area: 35.4 m2 (381 sq ft)
- Gross weight: 3,100 kg (6,834 lb)
- Powerplant: 1 × ČKD-built Hispano-Suiza 12Ydrs V-12 Liquid-cooled piston engine, 642 kW (861 hp)
Performance
- Maximum speed: 330 km/h (205 mph; 178 kn)
- Range: 1,000 km (621 mi; 540 nmi)
- Service ceiling: 9,000 m (29,528 ft)
- Rate of climb: 6.8 m/s (1,340 ft/min)
- Wing loading: 88 kg/m2 (18 lb/sq ft)
- Power/mass: 0.21 kW/kg
Armament
- Bombs: 200 kg (440 lb)
See also
 |
Wikimedia Commons has media related to Aero Vodochody aircraft. |
- Related development
- Related lists
