TsKB-30, S.V.IlyushinA ll-metal development of the TsKB-26.
It was armed three-seat aircraft. Its construction was an extreme development of wielded tube frames. Wielding quality was
monitored by X-Ray facilities, had very high quality - but required a lot of 'hand crafting'.
| Technical data | |
|---|---|---|
| Type | TsKB-30 | |
| Function | Bomber Prototype | |
| Year | 1936 | |
| Crew | 3 | |
| Engines | 2*760hp M-85/ Gnome-Rhone 14Krsd | |
| Length | 14.22m | |
| Wingspan | 21.44m | |
| Wing area | 65.6m2 | |
| Empty weight | 4200kg | |
| Loaded weight | 6250kg | |
| Wing load | 95kg/m2 | |
| Power load | 4.1kg/hp | |
| Speed (0m) | 335km/h | |
| Speed (3250m) | 409km/h | |
| Speed (landing) | 105km/h | |
| Armament | ||
| Bombs | 1000kg (external) | |
| Guns | 3*7.62 ShKAS | |
| Modified April 14, 1996
by Alexandre Savine; |
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