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Sukhoi Su-7

Military Aircraft

The Sukhoi Su-7, NATO reporting name Fitter-A, is a swept-wing supersonic fighter developed in the Soviet Union in 1955. It was designed first as a tactical low-level dogfighter and was not successful in that role, but the Su-7B series that followed became the main Soviet fighter-bomber and ground-attack aircraft of the 1960s. The first prototype, the S-1, used the new Lyulka AL-7 turbojet and first flew on 7 September 1955; after an afterburning version of the engine was fitted it set a Soviet speed record of 2,170 km/h in April 1956. The aircraft was rugged and simple, but the engine burned so much fuel that even short missions needed drop tanks on at least two hardpoints, which limited the payload. A total of 1,847 Su-7 and its variants were built, and India bought 140 in 1967.

Facts
Year
1955 1
Engine Class
Jet 1
Units Built
1847 1
Top Speed (km/h)
1150 1
Mass (kg)
8940 1
Maximum Mass (kg)
15,210 1
Comparison
Body Style
Aircraft (no road body style) 1
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Aviation, Modes
Source Sukhoi Su-7 (Wikipedia)

Of Make

Source Sukhoi Su-7 (Wikipedia)
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Source Sukhoi Su-7 (Wikipedia)Lead
Quote, Lead
is a swept wing, supersonic fighter aircraft developed by the Soviet Union in 1955.

Originated In

Also in Geography Atlas: where this subject originated.

Source Sukhoi Su-7 (Wikipedia)Lead
Quote, Lead
is a swept wing, supersonic fighter aircraft developed by the Soviet Union in 1955.
Sources
1. Sukhoi Su-7 (Wikipedia)
  • Design and development
    The S-1 first flew on 7 September 1955
  • Specifications
    Powerplant: 1 × Lyulka AL-7F-1 afterburning turbojet, 66.6 kN (15,000 lbf) thrust dry, 94.1 kN (21,200 lbf) with afterburner
  • Operational history
    A total of 1,847 Su-7 and its variants were built.
  • Lead
    is a swept wing, supersonic fighter aircraft developed by the Soviet Union in 1955.
  • Specifications, maximum speed
    Maximum speed: 1,150 km/h (710 mph, 620 kn) / 0.94 at sea level
  • Specifications, empty weight
    Empty weight: 8,940 kg (19,709 lb)
  • Specifications, maximum takeoff weight
    Max takeoff weight: 15,210 kg (33,532 lb)
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