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Mikoyan-Gurevich I-7

Supersonic and Experimental Aircraft

The I-7 was the second of three linked experimental fighter prototypes built by the Mikoyan-Gurevich bureau in the Soviet Union in the mid and late 1950s, between the I-3 and the I-75. It was meant as a Mach 2 class interceptor and as one component of the automated Uragan-1 air defence system of the PVO, in which ground radar and a control computer would steer the aircraft to its target with the pilot only as a backup. When the Klimov VK-3 engine of the I-3 was cancelled, the single I-3 airframe was rebuilt with a Lyulka AL-7 afterburning turbojet and a much longer fuselage, a step that marked the move from the MiG-19 family toward the MiG-21. After 19 flights the prototype was rebuilt again as the I-75.

Facts
Year
1957 1
Engine Class
Turbojet 1
Status
Prototype 1
Units Built
1 1
Mass (kg)
7952 1
Maximum Mass (kg)
11,540 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Mikoyan-Gurevich I-7 (Wikipedia)

Of Make

Source Mikoyan-Gurevich I-7 (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Mikoyan-Gurevich I-7 (Wikipedia)Lead, maker
Quote, Lead, maker
The Mikoyan-Gurevich I-7 was a development of the Mikoyan-Gurevich I-3 experimental fighter

Originated In

Also in Geography Atlas: where this subject originated.

Source Mikoyan-Gurevich I-7 (Wikipedia)Lead, country of origin
Quote, Lead, country of origin
the Soviet defense system
Sources
1. Mikoyan-Gurevich I-7 (Wikipedia)
  • Lead, aircraft type (body style)
    was a development of the Mikoyan-Gurevich I-3 experimental fighter
  • Operational history, 13th flight of the prototype
    On 21 June 1957, the sole prototype I-7U suffered damage when the starboard landing gear strut failed as the aircraft landed on its 13th flight.
  • Specifications (I-7U), powerplant
    Lyulka AL-7F afterburning turbojet
  • Specifications (I-7U), empty weight
    Empty weight: 7,952 kg (17,531 lb)
  • Specifications (I-7U), maximum take-off weight
    Max takeoff weight: 11,540 kg (25,441 lb)
  • Operational history, prototype
    the sole prototype I-7U
  • Lead, maker
    The Mikoyan-Gurevich I-7 was a development of the Mikoyan-Gurevich I-3 experimental fighter
  • Lead, country of origin
    the Soviet defense system
  • In Group: Experimental Jet Research Aircraft, Lead, aircraft type
    was a development of the Mikoyan-Gurevich I-3 experimental fighter
  • Exemplifies: Aviation, Lead, aircraft type (exemplifies)
    was a development of the Mikoyan-Gurevich I-3 experimental fighter
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