1937 experimental aircraft
G-23 Komsomolyets 2
The Gribovsky G-23 Komsomolyets 2 (Russian: Грибовский Г-23 Комсомолец 2) was a two-seat, single aircraft originally intended to explore the potential of a car-derived, water cooled inline engine for light aviation. It was built in the USSR in the 1930s. A second example was fitted with two different engines of greater power.
Summary from Wikipedia licensed under CC BY-SA.
- Manufacturer
- Vladislav Gribovsky
- Country of origin
- Soviet Union
Specifications
- Cruise speed
- 93 kt
- Max speed
- 97 kt
- Range
- 243 nm
- Service ceiling
- 26,198 ft
- Rate of climb
- 11.7 ft/min
- Powerplant
- M-11Ye 5-cylinder radial engine
- Engines
- 1
- Seats
- 2
- Length
- 34.4 ft
- Wingspan
- 36.1 ft
- Number built
- 2
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.