Mikoyan-Gurevich I-75


The Mikoyan-Gurevich I-75 was the final design of a series of three experimental swept-wing interceptors developed from the Mikoyan-Gurevich I-3 airframe developed by the Mikoyan-Gurevich design bureau in the Soviet Union in the mid-late 1950s. 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.

Design and development

The I-75 was a re-engined and radar-equipped version of the experimental I-7 Mach 2 class aircraft. Work on the I-7U started in early 1956, as a development of the proposed Klimov VK-3 turbojet powered I-3 prototype fighter. The airframe of the I-3 was modified for the larger and more powerful Lyulka AL-7F after-burning turbojet engine. A short test flight programme ended on 24 January 1958, after which the prototype was rebuilt into the I-75 by fitting an AL-7F-1 that delivered "dry" thrust of 6240 kg and 9215 kg with afterburner and modifying the nose to accept the Uragan-5 radar intercept system.
The maiden flight of I-75 took part on 28 April 1958. The Uragan-5B radar was fitted on 15 May 1958 and the tests continued from 25 December 1958.
Despite its excellent performance the I-75 constantly suffered from development delays and the I-75 programme was terminated on 11 May 1959.
Production contracts were placed for the contemporary Sukhoi T-43, as Sukhoi were able to develop this interceptor faster due to its high commonality with the Su-7 tactical fighter.
The armament of the I-75 consisted of two beam-riding long-range Kaliningrad K-8 missiles. So equipped, I-75 became a part of the Uragan automated interception system for which it served as a testbed for some time.
The Uragan-5 was the first Soviet radar system with head-on attack capability; maximum detection range was and acquisition range was up to.
The Uragan complex was designed to automatically guide the interceptor to its target, perform the attack, and withdrawal from action. Apart from the radar and the aircraft, the system consisted of a range ground radar, digital control computer, data acquisition and processing equipment, and an autopilot. The system was expected to be able to intercept bombers flying at 10 to altitude at 1600–2000 km/h; the interception was to take place within a radius from the aircraft base.

Specifications