Ilyushin Il-54

Last updated
Il-54
Il-54-sila-1.jpg
Three-quarter view of the second Il-54 prototype
RoleBomber
National originSoviet Union
Manufacturer Ilyushin
First flight3 April 1955
Number built2

The Il-54 was a transonic bomber developed in the USSR in the 1950s. Only two examples were built before the project was abandoned.

Contents

Design and development

The Council of Ministers issued a directive to OKB-115, for a transonic bomber prototype to be submitted for State Acceptance Trials in July 1954. The design of this bomber went through several stages before settling on the final configuration. [1]

The Il-54, as built, had a very thin 45 degree swept wing with anhedral, which was shoulder-mounted on the fuselage. The Lyulka AL-7 engines were housed in slim, pylon mounted, pods at approximately 1/3 span. Because the wings and engine nacelles were too small to house a conventional undercarriage, the Il-54 used a bicycle undercarriage arrangement, with nose and main gear units on the centreline of the aircraft, at each end of the bomb bay. This arrangement meant a conventional rotating takeoff would be impossible. To enable the Il-54 to take off, in a reasonable runway length, the main gear knelt and the nose gear extended to give the ideal angle of incidence for takeoff (10 degrees). [1]

Flight trials of the Il-54 commenced in April 1955 with test pilot Vladimir Kokkinaki at the controls. Difficult handling during the landing run was rectified by modifying the undercarriage. [1]

Production of the Il-54 was not proceeded with, due to competition from Yak-25 derivatives, and the belief that crewed aircraft would soon be replaced by missiles. [1]

Booked to fly in the flypast at Tushino Airfield in 1956, the Il-54 was dropped from the flying programme. The aircraft was then shown to a US military delegation at Kubinka. The delegation was told that the Il-54 was the Il-149, as part of a deception programme. As a result, the Il-54 was assigned far more importance than it actually warranted, and was assigned the NATO reporting name ("Blowlamp") after it had ceased flying. [1]

Variants

Datafrom:OKB Ilyushin [1]

Specifications (Il-54)

Data from OKB Ilyushin [1]

General characteristics

40,660 kg (89,640 lb) (2nd prototype)
2x Lyulka AL-7F 98.1 kN (22,100 lbf) with afterburning (2nd prototype)

Performance

1,250 km/h (780 mph; 670 kn) at 5,000 m (16,000 ft) (2nd prototype)
14,000 m (46,000 ft) (2nd prototype)

Armament

See also

Aircraft of comparable role, configuration, and era

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References

  1. 1 2 3 4 5 6 7 Gordon, Yefim; Komissarov, Dmitriy and Sergey (2004). OKB Ilyushin: A History of the Design Bureau and its Aircraft. London: Ian Allan. pp. 150–154. ISBN   1-85780-187-3.