T he VKh used two Anatra D fuselages, joined
by a new wing (still using elements of the Anade wing). Left fuselage was occupied by pilot,
the right one - observer. Gunner was located in nacell attached to the center of the upper wing, providing excellent defence.
Later crew was increased to 6.
| Technical data | ||||
|---|---|---|---|---|---|
| Type | Anadwa VKh | Anadwa Salmson | Khioni-4 | ||
| Function | light bomber | ||||
| Year | 1916 | 1917 | 1921 | ||
| Crew | 3 | 6 | ? | ||
| Engines | 2*100hp Monosaupape | 2*140hp Salmson | 2*160hp Salmson | ||
| Length | 7.7m | 8.1m | 8.1m | ||
| Wingspan | 19.0m | 19.1m | 19.1m | ||
| Wing area | 62.0m2 | 62.0m2 | 62.0m2 | ||
| Empty weight | - | 1280kg | 1300kg | ||
| Loaded weight | - | 1930kg | 2100kg | ||
| Wing load | - | 31.2kg/m2 | 34.0kg/m2 | ||
| Power load | - | 6.9kg/hp | 6.5kg/hp | ||
| Maximum Speed | - | 140km/h | 140km/h | ||
| Ceiling | - | 4000m | 4400m | ||
| Climb | |||||
| 1000m | - | 7.6min | 7.7min | ||
| 2000m | - | - | 19min | ||
| 3000m | - | 34min | 34.5min | ||
| Endurance | 3.0h | - | |||
| Payload | |||||
| Total | 600kg | 650kg | 800kg | ||
| Modified January 25, 1996
by Alexandre Savine; |
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