Tomashevich I-110
| Tomashevich I-110 | |
|---|---|
| Type: | Fighter plane |
| Design country: | |
| Manufacturer: |
KB-29 |
| First flight: |
1942 |
| Commissioning: |
only prototype |
.svg){kind=small}
The Tomaschewitsch I-110 ( Russian Томашевич И-110 ) was a single-seat fighter from the time of the Second World War .
development
In 1942, during his imprisonment in his KB-29 design office in Siberia , Dmitri Tomaschewitsch developed a fighter and fighter bomb aircraft that differed considerably from the production aircraft of the time. Because of the high bomb load and the very strong armor, it had a very high mass. The aircraft had a special cooling system with a very noticeable, large air inlet under the propeller. At the end of 1942, test pilot Pyotr Stefanowski took off for the first flight with the type known as the I-110 . It showed some very good flight characteristics, but the series production was not ordered because both the airframe and the engine would have resulted in a complete change in production, which the tense war situation did not allow.
Technical specifications
| Parameter | Data |
|---|---|
| crew | 1 |
| Wingspan | 10.20 m |
| length | 9.91 m |
| Wing area | 18.75 m² |
| Empty mass | 3,285 kg |
| Takeoff mass | 3,980 kg |
| Engine | a Klimow - M-107P - V-engine |
| Starting power | 1,075 kW (1,462 hp) |
| Top speed | 610 km / h at an altitude of 6,200 m |
| Ascent time to 5,000 m altitude | 7 min |
| Range | 1,050 km |
| Summit height | 10,000 m |
| Armament | a 20 mm SchWAK cannon in the propeller shaft and two 12.7 mm MG UBS above the engine
|
| Bomb load | 500 kg |
See also
Web links
- И-110. Retrieved June 30, 2016 (Russian).