Fightersexperimental interceptor designed by Mikoyan-Gurevich
I-75
The Mikoyan-Gurevich I-75 was the final design of a series of three experimental swept-wing interceptors developed in the Soviet Union in the mid-late 1950s by the Mikoyan-Gurevich design bureau from their Mikoyan-Gurevich I-3 airframe. All the aircraft in the I-3 program were affected by delays in the development of the Klimov VK-3 turbojet engine, its cancellation and ultimate replacement by the Lyulka AL-7F turbojet engine.
Summary from Wikipedia licensed under CC BY-SA.
- Manufacturer
- Russian Aircraft Corporation MiG
- Category
- Fighters
- Country of origin
- Soviet Union
- First flight
- 1958-01-01
Specifications
- Cruise speed
- 1,200 kt
- Max speed
- 1,200 kt
- Range
- 790 nm
- Service ceiling
- 69,000 ft
- Max takeoff weight
- 25,287 lb
- Empty weight
- 25,089 lb
- Powerplant
- Lyulka AL-7F-1 afterburning turbojet
- Engines
- 1
- Seats
- 1
- Length
- 55.7 ft
- Wingspan
- 32.7 ft
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.