Mikoyan-Gurevich I-211
The Mikoyan-Gurevich I-211 was a prototype high-altitude Soviet fighter aircraft built during World War II. It was a version of the Mikoyan-Gurevich I-210, itself a variant of the Mikoyan-Gurevich MiG-3, fitted with a Shvetsov ASh-82F radial engine. Its development was quite prolonged, although successful, but by the time it finished its manufacturer's trials in early 1944 there was no need for a high-altitude fighter and it was not worth reducing the production of existing fighters to convert a factory over to the I-211.
Summary from Wikipedia licensed under CC BY-SA.
- Manufacturer
- Russian Aircraft Corporation MiG
- Category
- Fighters
- Country of origin
- Soviet Union
- First flight
- 1943-02-12
Specifications
- Cruise speed
- 360 kt
- Max speed
- 360 kt
- Range
- 510 nm
- Service ceiling
- 37,300 ft
- Rate of climb
- 750 ft/min
- Max takeoff weight
- 6,768 lb
- Empty weight
- 5,710 lb
- Powerplant
- Shvetsov M-82F
- Engines
- 1
- Seats
- 1
- Length
- 26 ft
- Wingspan
- 33 ft
- Height
- 12 ft
- Number built
- 1
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.