FMA IA 36 Cóndor

Source: Wikipedia, the free encyclopedia.
I.A. 36 Cóndor
IA 36 wind tunnel model
Role Narrow-body jet airliner
Manufacturer
FMA/IAME
Designer Kurt Tank
First flight Not flown
Status Cancelled

The IA 36 Cóndor (English:

Fábrica Militar de Aviones
”. It was cancelled in 1958, with no prototypes built, but a full size wood mockup.

Design and development

Work on the IA 36 Cóndor project started in late 1951 by a team led by the German engineer

Juan Domingo Perón, deposed in 1955 by the now quite infamous Revolución Libertadora uprising.[1]

The projected aircraft would have been powered by five Rolls-Royce "Nene II" turbojets arranged in an annular configuration around the rear fuselage, as in Messerschmitt P.1110 and Heinkel He 211; however it was planned to replace those with lighter and more powerful engines in later versions.[2] The design would have accommodated 32 to 40 passengers; the maximum speed was expected to be 950 km/h (590 mph); in comparison, the contemporary

aerodynamic efficiency. The wingspan was 34 m (112 ft); and the estimated range was 5,000 km (3,100 mi; 2,700 nmi).[1]

Specifications

Data from [1]

General characteristics

  • Crew: 3-4
  • Capacity: 32-40 passengers
  • Wingspan: 34 m (111 ft 7 in)
  • Powerplant: 5 × Rolls-Royce Nene centrifugal-flow turbojet engines

Performance

  • Maximum speed: 950 km/h (590 mph, 510 kn)
  • Range: 5,000 km (3,100 mi, 2,700 nmi)

See also

Aircraft of comparable role, configuration, and era

Related lists

  • List of jet airliners

References

Notes

  1. ^ a b c "Aviones fabricados y proyectados desde 1943 hasta la Revolución Libertadora – I.A.36 Cóndor" (in Spanish). Archived from the original on 2 April 2012. Retrieved 20 March 2012.
  2. .

Further reading

  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.

External links