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Fairchild J44

The Fairchild J44 was a small expendable turbojet developed in the 1940s by the Fairchild Engine Division.

Design and development
The Fairchild Engine Division (previously the Ranger Aircraft Engine Division of the Fairchild Engine & Aircraft Corporation) began development of the J44 in 1947. It was used in target drones, missiles, and as jet boosters on several aircraft types. ==Applications==
Variants
Data from: Aircraft engines of the World 1953, Flight 20 March 1959 :AERO ENGINES 1959 . . ., Aircraft engines of the World 1957 ;XJ44: Prototypes of the J44 ;J44-R-1:United States Air Force (USAF) engine, similar to the United States Navy (USN) -6, . ;J44-R-2:Same as -6 but with different installation. ;J44-R-3: Longer life - Fairchild C-123 Provider wing-tip boosters. ;J44-R-6: USN version, . ;J44-R-12: expendable. ;J44-R-20B:Ryan Firebee. ;J44-R-24:Fairchild Petrel. ;J44-R-26: company sponsored variant. ;FT-101E:Commercial version of -3. ;FT-101-G:Commercial version with return oil system. ==Specifications(J44-R-3)==
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