| Technical data | |
|---|---|
| Type | BOK-5 |
| Year | 1937 |
| Function | Experimental |
| Engine | 1x100hp M-11 |
| Wing Span | 9.86m |
| Wing Area | 23.15m2 |
| Length | 4.37m |
| Empty Weight | 596kg |
| Loaded Weight | 764kg (90kg fuel) |
| Max Speed | 174km/h |
| Landing speed | 85km/h |
| Take off/Landing Roll | 120/200m |
| Ceiling | 4,850m |
| Range | 600km |
| Endurance | 4h |
BOK-5, V.A.Chizhevskij
 |
The BOK-5 was an light-weight (duralumin/fabric) experimental tailless aircraft (powered single-seat glider) with full-span tandem control surfaces along the trailing edge. It had a short stubby fuselage with a radial engine and a conventional fin.
Flown by test-pilots Stefanovskij and Nukhtikov;
Load factor +8 (!)
Thanks to A.Gretchihine Trivia-8 Solution, where the picture was found and a lot of technical parameters
-
More Links...
- BOK-5
- BOK-5 (Slovak)
