| Manufacturer |
Vladimir Gribovsky |
Australian Aircraft Consortium pty. |
| Description |
The Gribovsky G-23 Komsomolyets 2 () was a two-seat, single aircraft originally intended to explore the potential of a car-derived, water cooled inline engine for light aviation. |
The AAC Wamira was a turboprop military trainer aircraft, designed for the Royal Australian Air Force (RAAF) by the Australian Aircraft Consortium (AAC). |
| First Flight |
1937-02-01 |
|
| Designer |
Vladislav Gribovsky |
Australian Aircraft Consortium pty. |
| Type |
|
Trainer aircraft |
| Length (m) |
10.5 |
10.2 |
| Height (m) |
|
3.51 |
| Max Speed (km/h) |
179 |
462.9996 |
| Cruise Speed (km/h) |
|
333.3597 |
| Min Speed (km/h) |
|
105.5639 |
| Max Ceiling (m) |
7985 |
9692.64 |
| Rate of Climb (m/s) |
|
14.0208 |
| Armament |
|
4x underwing hardpoints, stressed for 250 kg each inboard and 150 kg each outboard |
| Endurance (h) |
|
3 |
| National Origin |
Soviet Union |
|
| Number Built |
2 |
0 |
| Powerplant Description |
1 × M-11Ye 5-cylinder radial engine, 112 kW (150 hp) each |
1 × Pratt & Whitney Canada PT6A-25C turboprop, 559 kW (750 hp) each |
| Primary Users |
|
Royal Australian Air Force |
| Status |
|
Cancelled 1986 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Gribovsky_G-23 |
en.wikipedia.org/wiki/AAC_Wamira |
| Flat Wing Span (m) |
11 |
11 |
| Flat Wing Area (m²) |
14.9 |
20 |
| Aircraft Engine |
|
Pratt & Whitney Canada PT6 |
| Number of Engines |
1 |
1 |