Gribovsky G-23 Komsomolyets 2
Vladislav Gribovsky · Soviet Union · first flew 1937 · light aircraft
The Gribovsky G-23 Komsomolyets 2 was a two-seat experimental sports aircraft built in the USSR in the 1930s.
Recognition (WEFT)
| W — Wings | Low-mounted, tapered |
|---|---|
| E — Engines | 1 × piston, nose-mounted |
| F — Fuselage | Low-wing cantilever monoplane with a flat-sided fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Low-wing cantilever monoplane with a flat-sided fuselage
- Long dorsal headrest fairing and elliptical vertical tail
- Fixed tailskid undercarriage with each main wheel on a single faired leg
The original G-23 had a radiator under the nose and a low-set propeller, with two tandem seats.
Specifications
- The Gribovsky G-23 Komsomolyets 2 has a length of 10.5 m (34 ft).
- It has a wingspan of 11 m (36 ft).
- Its maximum speed is 179 km/h (111 mph).
- Typical crew: 2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
It was designed to test the suitability of the GAZ-M-60, a car-derived water-cooled engine, for light aircraft. It was much like the single-seat G-22 but with a 25 per cent greater span and an extra tandem seat.
Variants
The G-23 flew in 1937 with the GAZ-M-60, the G-23bis in 1938 with a 150 hp M-11Ye radial, and the G-23bis-GAZ in late 1938 with a GAZ-11. The figures here are for the G-23bis.
Where you'll see it
In summer 1937 it flew a 2,584 km out-and-return race from Moscow to Sebastopol in 21 hours, configured as a single-seater.
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- Gribovsky G-25
- Gribovsky G-22
- Gribovsky G-28
- Gribovsky G-8
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