Ikarus Aero 2
Ikarus Aero 2 | |
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Type: | Trainer aircraft |
Design country: | |
Manufacturer: | |
First flight: |
1940 |
Commissioning: |
1948 |
Number of pieces: |
248 or 380 |
The Ikarus Aero 2 ( Serbian - Cyrillic Икарус Аеро 2 ) was a two-seat beginner's training aircraft from the Yugoslav manufacturer Ikarus .
history
Due to a demand of the “Royal Yugoslav Air Force” before the Second World War , the Aero 2 was developed to replace the outdated Fizir FN biplane training aircraft. The Aero 2 was developed by Boris Cijan and Dorde Petkovic . The prototype flew in 1940, but development was interrupted due to the events of the war and only resumed after the now Yugoslav " Air Force and Air Defense " was formed. 248 (380 according to other data) copies were built and were in use from 1948 to 1959.
construction
The Aero 2 was a conventional low-wing aircraft with a fixed tail wheel landing gear . Teacher and student sat one behind the other. The aircraft was from a de Havilland Gipsy Major - piston engine driven.
Versions
- Aero 2B
- Open cockpit with a 108 kW de Havilland Gipsy Major piston engine
- Aero 2BE
- Closed cockpit with a 108 kW de Havilland Gipsy Major piston engine
- Aero 2C
- Open cockpit with a 119 kW Walter Minor 6-III piston engine
- Aero 2D
- Closed cockpit with a 119 kW Walter Minor 6-III piston engine
- Aero 2E
- Closed cockpit with a 119 kW Walter Minor 6-III piston engine
- Aero 2F
- Open cockpit with a 119 kW Walter Minor 6-III piston engine
- Aero 2H
- Seaplane version equipped with two floats with a 119 kW Walter Minor 6-III piston engine
use
Technical specifications
Parameter | Data (2B) |
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crew | 1-2 |
length | 8.45 m |
span | 10.5 m |
height | 2.80 m |
Wing area | 17.4 m² |
Empty mass | 564 kg |
Max. Takeoff mass | 996 kg |
Top speed | 208 km / h |
Service ceiling | 4500 m |
Range | 680 km |
Engines | 1 × piston engine de Havilland Gipsy Major with 108 kW (147 PS ) |
See also
Web links
Individual evidence
- ↑ a b Ugolok Neba
- ↑ Orbis 1985, page 36