Pratt & Whitney J75

The Pratt & Whitney J75 (civilian designation: JT4A) is an axial-flow turbojet engine first flown in 1955. A two-spool design in the 17,000 lbf (76 kN) thrust class, the J75 was essentially the bigger brother of the Pratt & Whitney J57 (JT3C). It was known in civilian service as the JT4A, and in a variety of stationary roles as the GG4 and FT4.

Design and development
In military use, the J75 was used on the Convair F-106 Delta Dart, Lockheed U-2, and Republic F-105 Thunderchief. It was also utilized in the prototype and experimental Avro Canada CF-105 Arrow, Lockheed A-12, Martin P6M-2 SeaMaster, North American YF-107, and Vought XF8U-3 Crusader III.

Before the arrival of the Pratt & Whitney JT3D turbofan engine, the JT4A was used to power certain Boeing 707 and Douglas DC-8 models, bringing improved field performance in the medium-range Boeing 707-220 and Douglas DC-8-20, and intercontinental range in the Boeing 707-320 and the Douglas DC-8-30. By late 1959, P&W had considered introducing a turbofan version of the J75, which was to have tentatively been named the TF75 or JT4D. Apparently, little interest was shown by the aircraft industry, so the variant was dropped.

Marine & power generation
After its relatively short lifetime in the aircraft role, the JT4A found more enduring use in the naval role, where the FT4 was produced in a variety of models between 18,000 and 22,000 hp. Well-known uses include the first all-turbine warships, the Canadian Iroquois-class destroyers, as well as the United States Coast Guard's Hamilton-class cutters, the 1970s-built icebreakers Polar Sea and Polar Star (each 3 engines in CODOG configuration), and it was considered for the US Navy's Asheville-class gunboat. The same basic powerplant saw much wider use as a peak demand power turbine running on natural gas. From its introduction in 1960 over 1,000 FT4s have been sold, with many of them still in operation for electrical generation. Outdated by modern standards, refits are available that add catalytic converters to lower their emissions.

Variants

 * J75-P-1:
 * J75-P-3: 16,470 lbf thrust
 * J75-P-5: 17,200 lbf thrust
 * J75-P-9:
 * J75-P-11:
 * J75-P-13B: 17,000 lbf thrust
 * J75-P-15W: 24,500 lbf afterburning thrust
 * J75-P-17: 24,500 lbf afterburning thrust
 * J75-P-19: 24,500 lbf afterburning thrust
 * J75-P-19W: 26,500 lbf afterburning thrust with water injection
 * JT4A-3: 15,800 lbf
 * JT4A-4: 15,800 lbf
 * JT4A-9: 16,800 lbf
 * JT4A-11: 17,500 lbf thrust
 * JT4A-29: (J75-P-19W) 26,500 lbf afterburning thrust with water injection

Applications



 * J75
 * Avro Canada CF-105 Mk1 Arrow (interim for test flights)
 * Convair F-106 Delta Dart
 * Lockheed A-12 (interim for test flights)
 * Lockheed U-2
 * Martin P6M-2 SeaMaster
 * North American F-107
 * Republic F-105 Thunderchief
 * Vought XF8U-3 Crusader III


 * JT4A
 * Boeing 707 (specifically, the 707-220 and 707-320)
 * Douglas DC-8 (specifically, the DC-8-20 and DC-8-30)