Antonov A-11
Antonov A-11 | |
---|---|
Antonov A-11 |
|
Type: | Glider |
Design country: | |
Manufacturer: | |
First flight: |
May 12, 1958 |
Production time: |
1958-1964 |
Number of pieces: |
≈ 150 |
The Antonov A-11 was a Soviet glider .
development
The machine was approved for aerobatics and the instrumentation was sufficient to break through clouds. The first flight took place on May 12, 1958. A type with a reduced wingspan developed parallel to the A-11 was the Antonov A-13 .
construction
The middle-decker made of metal (self-supporting shell construction) had a V-tail unit as a special feature . This and part of the wing were covered with fabric, otherwise the planking was also made of metal. The landing gear consists of a retractable main wheel and a tail spur. There is also a runner under the bow. Curved flaps serve as landing flaps, and there are also spoilers in the wings. There were rub strips on the wing ends.
Technical specifications
Parameter | Data |
---|---|
Years of construction | 1958-1964 |
Manufacturer | Antonov |
span | 16.50 m |
length | 6.00 m |
height | 1.62 m |
Wing area | 12.15 m² |
Wing extension | 22.40 |
profile | ZAGI P-IIIa |
Glide ratio | 34 at 97 km / h |
Slightest sinking | 0.74 m / s at 97 km / h |
Empty mass | 294 kg |
Preparation mass | 310 kg |
Payload | 100 kg |
Takeoff mass | 410 kg |
Wing loading | 33.70 kg / m² |
Top speed | 350 km / h (maximum permissible) 140 km / h in aircraft tow 100 km / h in winch tow |
Minimum speed | 60 km / h |
crew | 1 |
See also
literature
- Heinz A. F. Schmidt: Soviet planes . Transpress , Berlin 1971, p. 185 .
- Heinz A. F. Schmidt: Gliders . In: Aerotype . Transpress, Berlin 1969, p. 90/91 .
- Heinz A. F. Schmidt: Airplanes from all over the world . Volume II. Transpress, Berlin, p. 126 .
Web links
Commons : Antonov A-11 - Collection of images, videos and audio files
Individual evidence
- ^ Rudolf Höflinger: Antonov. Airplanes since 1946. Motorbuch, Stuttgart 2013, ISBN 978-3-613-03518-8 , p. 10