Exactly 65 years ago, in October 1960, the Su-9 interceptor fighter was adopted into service by a government decision. This event marked a new stage for the P.O. Sukhoi Design Bureau, marking the first model of new combat aviation adopted into service after the restoration of the Design Bureau. In addition, the Su-9 became part of the first domestic Su-9-51 intercept aviation complex, which was characterized not only by the aviation component, but also by the Vozdukh-1 ground guidance system.
The development of this project lasted more than seven years: the task was set in August 1953, the first prototype T-3 flew in May 1956, and state tests of the interceptor modification under the designation T-43 were carried out from December 1958 to April 1960.
The Su-9 (originally known as the T-3) was mass-produced from 1958 to 1962 at two aircraft factories: No. 153 in Novosibirsk and No. 30 in Moscow. During this time, 1066 units were manufactured, including 50 Su-9U combat trainers.
In the initial stages, in 1959–1960, the aircraft were used both in the Air Force and in the Air Defense Forces, but since 1960 they were transferred exclusively to the aviation of the Air Defense Forces. These aircraft were not exported, and at the peak of their deployment, in the early 60s, the Su-9 was in service with 29 fighter aviation regiments, stationed only on the territory of the Soviet Union.
The aircraft was first demonstrated to the general public at an air parade held on July 9, 1961 in Tushino.
These aircraft remained in service in the Soviet Union until 1980, when they were finally decommissioned. Until the early 70s, when the MiG-25 began to enter the army, the Su-9s were in fact the highest-altitude and fastest aircraft in the USSR. This was confirmed by world speed and altitude records set between 1959 and 1962 by test pilots V.S. Ilyushin, A.A. Koznov and B.M. Adrianov.
Su-9 (NATO codification: Fishpot) is a Soviet single-engine all-weather interceptor fighter. One of the first Soviet aircraft with a delta wing, the world's first interceptor fighter, created as an integral part of a single interception complex.
Technical characteristics:
- maximum speed: 2,230 km/h at an altitude of 12,000 m;
- practical range: without PTB — 1,350 km, with PTB — 1,800 km;
- practical ceiling: 20,000 m;
- rate of climb: 200 m/s;
- takeoff distance: 1,200 m;
- run distance: 1,250 m (without braking parachute).
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