Douglas C-132

C-132
Artist's concept of the C-132
Role Cargo transport
National origin United States
Manufacturer Douglas Aircraft Company
Number built 0
Developed from C-124 Globemaster II

The Douglas C-132 was a proposed transport aircraft, based on the company's C-124 Globemaster II. However, it did not get past the mock-up stage. The C-132 was to be powered by four 15,000 shp (11,000 kW) Pratt & Whitney XT57 (PT5) turboprops, mounted on a swept wing. One XT57 was installed in the nose of a C-124 (AF serial number 52-1069) for testing.[1][2] Projected speed was to be 418 knots (774 km/h) with a range of 2,200 nautical miles (4,100 km) and a maximum payload of 137,000 pounds.[3]

Specifications (C-132)

Data from The Encyclopedia of World Aircraft[4]

General characteristics

Performance

See also

Related development


References

Wikimedia Commons has media related to Douglas C-132.
  1. Francillon, René J. McDonnell Douglas aircraft since 1920 (Putnam, 1979), p.470.
  2. Connors, p.294
  3. Remembering An Unsung Giant - The Douglas C-133 Cargomaster and Its People
  4. Donald, David, ed. (1997). The Encyclopedia of World Aircraft. Prospero Books. p. 355. ISBN 1-85605-375-X.