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Douglas C-132 : ウィキペディア英語版 | Douglas C-132 __NOTOC__
The Douglas C-132 was a proposed transport aircraft, based on the company's C-124 Globemaster II. Design studies began in 1951 but the project was cancelled in 1957 by the USAF. No prototype was built and the project did not get past the mock-up stage. The C-132 was to be powered by four Pratt & Whitney XT57 (PT5) turboprops, mounted on a swept wing. An air refueling version, the XKC-132 was also proposed, but it would only have utilized the probe and drogue (P&D) air refueling system and that system, used primarily by the US Navy, did not find favor with the USAF. One XT57 was installed in the nose of a C-124 (AF serial number 52-1069) for testing.〔Francillon, René J. ''McDonnell Douglas aircraft since 1920'' (Putnam, 1979), p.470.〕〔Connors, p.294〕 Projected speed was to be with a range of and a maximum payload of 137,000 pounds.〔(''Remembering An Unsung Giant - The Douglas C-133 Cargomaster and Its People'' )〕 ==Specifications (C-132) ==
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