T-3, P.O.Sukhoj


P
rototype of fighter-interceptor with delta-wing. Project started in 1953, when P.O.Sukhoj OKB was restored after 3 years break. T-3 was developed in parallel with swept-wing S-1 front-line fighter in a record short time, thanks for sharing of technologies and parts between the projects.
T-3 took off on 26 May 1956, with test-pilot V.N.Mahalin at controls. The T-3 had a circular fixed supersonic nose intake with a pointed radome above it for the search radar, and a second spherical radome for the tracking radar in the inlet ('Almaz' system). Swept tailplane was installed on fuselage empennage in the mid position.
Suggested armament consisted of two guided air-to-air missiles K-6 or K-7 (then under development). Flight trials and wind tunnel studies proved that radar housing induces too much drag. Problems and delays with K-6 and K-7 resulted in cancellation of projects, and armament of two early K-5M missiles (the only type in production) was found insufficient. Serious problems were caused by the engine: it was replaced four times during only 38 flight hours!
One prototype assembled, after trials (total 80 hours) re-built into T-43-1 with new radar in redesigned nose section and doubled armament.
PredecessorsModifications Developments
T-1
T-43
PT-7
PT-8

T-47

ReferencesLinks
  • Л.М.Кузьмина. Конструктор Сухой: "Су"-люди и самолеты. - М.:Воениздат, 1993. - 383 с.
  • Мы могли быть первыми. - Аэрофакт. Международный авиационый журнал на русском языке, 1993, №1, с. 24-25;
  • Н.Гордюков. Выход из тени. - Там же, с. 26-27, 30-34;
  • В.Павлов. Сверхзвуковые трубы всесоюзного оркестра.- Авиация и Время, 1998, №6, с.4-30;
  • Mir Aviatsii 2/1993
  • Experts contest, tour VI
  • T-3, Sukhoi
  • Russian Power Site
  • Technical data
    Type T-3
    Function Base Fighter design
    Year 1956
    Crew 1
    Engines 1*9060kg Lyulka Al-7F
    Length 16.75m
    Wingspan 58.43m
    Wing area 24.2m2
    Empty weight kg
    Loaded weight kg
    Wing load kg/m2
    Power load kg/hp
    Trust-to-Weight
    Speed at 0m km/h
    Speed at ?m 2100km/h
    Landing Speed km/h
    Landing Roll m sec
    Takeoff Roll m sec
    Turn time sec
    Range km
    Flight Endurance hmin
    Ceiling 18000m
    Climb
    1000m min
    Payload
    Fuel kg
    Armament
    Rockets 2*
    Created December 1996
    Modified January 26, 1999
    by Alexandre Savine
    Back to
    Main Gate